32292 Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 

York ACO Branch, 1600 Stewart Avenue, 

Suite 410, Westbury, NY 11590; telephone 

516–228–7300; email 9-avs-nyaco-cos@

faa.gov. 

(k) 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) Transport Canada Civil Aviation (TCCA) 

Emergency AD CF–2022–23, dated April 22, 

2022. 

(ii) [Reserved] 

(3) For TCCA Emergency AD CF–2022–23, 

contact TCCA, Transport Canada National 

Aircraft Certification, 159 Cleopatra Drive, 

Nepean, Ontario K1A 0N5, Canada; 

telephone 888–663–3639; email AD-CN@

tc.gc.ca; internet https://tc.canada.ca/en/ 

aviation. 

(4) You may view this material at the FAA, 

Airworthiness Products Section, Operational 

Safety Branch, 2200 South 216th St., Des 

Moines, WA. For information on the 

availability of this material at the FAA, call 

206–231–3195. 

(5) You may view this material that is 

incorporated by reference at the National 

Archives and Records Administration 

(NARA). For information on the availability 

of this material at NARA, email 

fr.inspection@nara.gov, or go to: https://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued on May 24, 2022. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2022–11660 Filed 5–26–22; 11:15 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–1172; Project 

Identifier MCAI–2021–00939–T; Amendment 

39–22051; AD 2022–11–01] 

RIN 2120–AA64 

Airworthiness Directives; Airbus SAS 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Airbus SAS Model A300 series 

airplanes, Model A300 B4–600, B4– 

600R, and F4–600R series airplanes, and 

Model A300 C4–605R Variant F 

airplanes (collectively called Model 

A300–600 series airplanes). This AD 

was prompted by reports of cracking in 

the main landing gear (MLG) support rib 

5 lower flange. This AD requires a onetime detailed inspection (DET) of the 

affected area, and applicable corrective 

actions, as specified in a European 

Union Aviation Safety Agency (EASA) 

AD, which is incorporated by reference. 

The FAA is issuing this AD to address 

the unsafe condition on these products. 

DATES: This AD is effective July 5, 2022. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of July 5, 2022. 

ADDRESSES: For material incorporated 

by reference (IBR) in this AD, contact 

EASA, Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; telephone +49 221 

8999 000; email ADs@easa.europa.eu; 

internet www.easa.europa.eu. You may 

find this IBR material on the EASA 

website at https://ad.easa.europa.eu. 

You may view this material at the FAA, 

Airworthiness Products Section, 

Operational Safety Branch, 2200 South 

216th St., Des Moines, WA. For 

information on the availability of this 

material at the FAA, call 206–231–3195. 

It is also available in the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–1172. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–1172; or in person at Docket 

Operations between 9 a.m. and 5 p.m., 

Monday through Friday, except Federal 

holidays. The AD docket contains this 

final rule, the mandatory continuing 

airworthiness information (MCAI), any 

comments received, and other 

information. The address for Docket 

Operations is U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE, 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aerospace Engineer, Large 

Aircraft Section, FAA, International 

Validation Branch, 2200 South 216th 

St., Des Moines, WA 98198; telephone 

and fax 206–231–3225; email 

dan.rodina@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

EASA, which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2021–0190, 

dated August 17, 2021 (EASA AD 2021– 

0190) (also referred to as the MCAI), to 

correct an unsafe condition for certain 

Airbus SAS Model A300, A300–600, 

and A300–600ST airplanes. Model 

A300–600ST airplanes are not 

certificated by the FAA and are not 

included on the U.S. type certificate 

data sheet; this AD therefore does not 

include those airplanes in the 

applicability. 

The FAA issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain Airbus SAS Model 

A300 series airplanes and Model A300– 

600 series airplanes. The NPRM 

published in the Federal Register on 

January 12, 2022 (87 FR 1703). The 

NPRM was prompted by reports of 

cracking in the MLG support rib 5 lower 

flange. The NPRM proposed to require 

a one-time DET of the affected area, and 

applicable corrective actions, as 

specified in EASA AD 2021–0190. 

The FAA is issuing this AD to address 

cracking of the MLG support rib 5 lower 

flange. This condition, if not detected 

and corrected, could affect the structural 

integrity of the airplane. See the MCAI 

for additional background information. 

Discussion of Final Airworthiness 

Directive 

Comments 

The FAA received a comment from 

FedEx. The following presents the 

comment received on the NPRM and the 

FAA’s response. 

Request for Allowance of Previously 

Approved Hardware 

FedEx requested that the FAA include 

a comment allowing previous Airbus 

Repair Design Approval Sheet (RDAS)- 

approved hardware that is different 

from the hardware specified in Airbus 

Alert Operators Transmission (AOT) 

A57W017–21 (which is referred to in 

EASA AD 2021–0190). FedEx noted that 

it had airplanes with different fasteners 

than those specified in a required for 

compliance (RC) step in Airbus AOT 

A57W017–21, and that those different 

fasteners were approved through an 

Airbus RDAS. FedEx added that Airbus 

provided configuration approval and 

structural acceptance of its proposed 

deviations to the fastener specifications 

through Airbus Statement of 

Airworthiness Compliance (ASAC) 

80955386/006/2021 Issue 1, dated 

August 25, 2021, and ASAC 08955386/ 

024/2022 Issue 1, dated February 25, 

2022. FedEx stated that adding such a 

provision in the proposed AD would 

eliminate the necessity for an alternative 

method of compliance (AMOC). 

The FAA concurs with FedEx’s 

request because the alternative method 

will provide an acceptable level of 


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Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 32293 

safety. The ASAC documents are 

equivalent to an AMOC approval. The 

FAA has redesignated paragraph (i)(1) of 

the proposed AD as paragraph (i)(1)(i) of 

this AD and added paragraph (i)(1)(ii) to 

this AD to specify that Airbus ASAC 

80955386/006/2021, Issue 1, dated 

August 25, 2021, and ASAC 80955386/ 

024/2022, Issue 1, dated February 25, 

2022, are approved as AMOCs for the 

corresponding provisions of this AD, for 

the airplanes identified in those ASACs 

only. 

Conclusion 

The FAA reviewed the relevant data, 

considered the comment received, and 

determined that air safety requires 

adopting this AD as proposed. 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. Accordingly, the FAA is 

issuing this AD to address the unsafe 

condition on these products. 

Related Service Information Under 1 

CFR Part 51 

EASA AD 2021–0190 specifies 

procedures for a DET of the affected 

area, a one-time fluorescent penetrant 

inspection (FPI) around some fastener 

holes in the affected area, and 

applicable corrective action(s) including 

crack repair. 

This material is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section. 

Costs of Compliance 

The FAA estimates that this AD 

affects 124 airplanes of U.S. registry. 

The FAA estimates the following costs 

to comply with this AD: 

ESTIMATED COSTS FOR REQUIRED ACTIONS

Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

23 work-hours × $85 per hour = $1,955 ..................................................................................... $0 $1,955 $242,420 

The FAA estimates the following 

costs to replace any cracked rib that 

would be required based on the results 

of any required actions and repair 

status. The FAA has no way of 

determining the number of aircraft that 

might need this on-condition action: 

ESTIMATED COSTS OF ON-CONDITION ACTIONS

Labor cost Parts cost Cost per product 

Up to 1,500 work-hours × $85 per hour = $127,500 ........................................................................................... $620,000 Up to $747,500. 

The FAA has received no definitive 

data on which to base the cost estimates 

for the repair specified in this AD. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. Subtitle VII: 

Aviation Programs, describes in more 

detail the scope of the Agency’s 

authority. 

The FAA is issuing this rulemaking 

under the authority described in 

Subtitle VII, Part A, Subpart III, Section 

44701: General requirements. Under 

that section, Congress charges the FAA 

with promoting safe flight of civil 

aircraft in air commerce by prescribing 

regulations for practices, methods, and 

procedures the Administrator finds 

necessary for safety in air commerce. 

This regulation is within the scope of 

that authority because it addresses an 

unsafe condition that is likely to exist or 

develop on products identified in this 

rulemaking action. 

Regulatory Findings 

This AD will not have federalism 

implications under Executive Order 

13132. This AD will not have a 

substantial direct effect on the States, on 

the relationship between the national 

government and the States, or on the 

distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Will not affect intrastate aviation 

in Alaska, and 

(3) Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

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

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive: 

2022–11–01 Airbus SAS: Amendment 39– 

22051; Docket No. FAA–2021–1172; 

Project Identifier MCAI–2021–00939–T. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective July 5, 2022. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the Airbus SAS 

airplanes, certificated in any category, 

without Airbus modification 11912 and 

identified in figure 1 to paragraph (c) of this 

AD. 


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32294 Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 

(d) Subject 

Air Transport Association (ATA) of 

America Code 57, Wings. 

(e) Unsafe Condition 

This AD was prompted by reports of 

cracking in the main landing gear (MLG) 

support rib 5 lower flange, inboard and 

outboard of Rib 5, on the right-hand and lefthand sides. The FAA is issuing this AD to 

address cracking of the MLG support rib 5 

lower flange. This condition, if not detected 

and corrected, could affect the structural 

integrity of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Requirements 

Except as specified in paragraph (h) of this 

AD: Comply with all required actions and 

compliance times specified in, and in 

accordance with, European Union Aviation 

Safety Agency (EASA) AD 2021–0190, dated 

August 17, 2021 (EASA AD 2021–0190). 

(h) Exceptions to EASA AD 2021–0190 

(1) Where EASA AD 2021–0190 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

(2) Where paragraph (3) of EASA AD 2021– 

0190 specifies to ‘‘accomplish those 

instructions accordingly’’ if any crack is 

detected, for this AD if any crack is detected, 

the crack must be repaired before further 

flight using a method approved by the 

Manager, Large Aircraft Section, 

International Validation Branch, FAA; or 

EASA; or Airbus SAS’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(3) The ‘‘Remarks’’ section of EASA AD 

2021–0190 does not apply to this AD. 

(i) Additional AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): 

(i) The Manager, Large Aircraft Section, 

International Validation Branch, FAA, has 

the authority to approve AMOCs for this AD, 

if requested using the procedures found in 14 

CFR 39.19. In accordance with 14 CFR 39.19, 

send your request to your principal inspector 

or responsible Flight Standards Office, as 

appropriate. If sending information directly 

to the Large Aircraft Section, International 

Validation Branch, send it to the attention of 

the person identified in paragraph (j) of this 

AD. Information may be emailed to: 9-AVSAIR-730-AMOC@faa.gov. Before using any 

approved AMOC, notify your appropriate 

principal inspector, or lacking a principal 

inspector, the manager of the responsible 

Flight Standards Office. 

(ii) Airbus Statement of Airworthiness 

Compliance (ASAC) 80955386/006/2021, 

Issue 1, dated August 25, 2021, and ASAC 

80955386/024/2022, Issue 1, dated February 

25, 2022, are approved as AMOCs for the 

corresponding provisions of this AD for the 

airplanes identified in those ASACs only. 

(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, Large Aircraft Section, 

International Validation Branch, FAA; or 

EASA; or Airbus SAS’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(3) Required for Compliance (RC): Except 

as required by paragraph (i)(2) of this AD, if 

any service information referenced in EASA 

AD 2021–0190 contains paragraphs that are 

labeled as RC, the instructions in RC 

paragraphs, including subparagraphs under 

an RC paragraph, must be done to comply 

with this AD; any paragraphs, including 

subparagraphs under those paragraphs, that 

are not identified as RC are recommended. 

The instructions in paragraphs, including 

subparagraphs under those paragraphs, not 

identified as RC may be deviated from using 

accepted methods in accordance with the 

operator’s maintenance or inspection 

program without obtaining approval of an 

AMOC, provided the instructions identified 

as RC can be done and the airplane can be 

put back in an airworthy condition. Any 

substitutions or changes to instructions 

identified as RC require approval of an 

AMOC. 

(j) Related Information 

For more information about this AD, 

contact Dan Rodina, Aerospace Engineer, 

Large Aircraft Section, FAA, International 

Validation Branch, 2200 South 216th St., Des 

Moines, WA 98198; telephone and fax 206– 

231–3225; email dan.rodina@faa.gov. 

(k) 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. 


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Figure 1 to paragraph (c): Affected airplanes by MSN 

Model 

A300 B2-1A, B2-1C, B2K-3C, 

B2-203, B4-2C, B4-103, and 

B4-203 airplanes 

A300 B4-601, B4-603, B4-620, 

and B4-622 airplanes 

A300 B4-605R and B4-622R 

airplanes 

A300 C4-605R Variant F 

airplanes 

A300 F4-605R and F4-622R 

airplanes 

Manufacturer Serial Number (MSN) 

075,080,090, 107,126,139,141,151,154,157, 

173,175,183,203,210,212,227,235,239,255, 

256,261,274,277,292,299,and302 

358,361,365,380,388,401,405,408,417,464, 

477,479,518,521,530,532,536,543,546,553, 

555,557,559,561,572,575,579,581,584,602, 

603,607,608,611,613,617,618,621,623,625, 

626,630,632,633,637,641,643,657,659,664, 

666,668,670,677,679,683,688,696,701,703, 

707,709,711,713,715,717,722,723,724,725, 

726,727,728,729,730,732,733,734,735,736, 

737,738,739,740,741,742,743,744,745,746, 

748,749,750,752,753,754,755,756,757,758, 

759,760,761,762,763,764,766,768,769,770, 

771,772,773,774,775,777,778,779,780,781, 

783, 789, 790, and 791 
Federal Register / Vol. 87, No. 104 / Tuesday, May 31, 2022 / Rules and Regulations 32295 

(i) European Union Aviation Safety Agency 

(EASA) AD 2021–0190, dated August 17, 

2021. 

(ii) [Reserved] 

(3) For EASA AD 2021–0190, contact 

EASA, Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; telephone +49 221 8999 

000; email ADs@easa.europa.eu; internet 

www.easa.europa.eu. You may find this 

EASA AD on the EASA website at https://

ad.easa.europa.eu. 

(4) You may view this material at the FAA, 

Airworthiness Products Section, Operational 

Safety Branch, 2200 South 216th St., Des 

Moines, WA. For information on the 

availability of this material at the FAA, call 

206–231–3195. 

(5) You may view this material that is 

incorporated by reference at the National 

Archives and Records Administration 

(NARA). For information on the availability 

of this material at NARA, email 

fr.inspection@nara.gov, or go to: https://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued on May 13, 2022. 

Gaetano A. Sciortino, 

Deputy Director for Strategic Initiatives, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2022–11538 Filed 5–27–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0787; Project 

Identifier MCAI–2021–00252–T; Amendment 

39–22048; AD 2022–10–10] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc., Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Bombardier, Inc., Model CL–600–1A11 

(600), CL–600–2A12 (601), and CL–600– 

2B16 (601–3A, 601–3R, and 604 

Variants) airplanes. This AD was 

prompted by a report of a wing stall 

(wing drop/un-commanded roll) during 

a landing flare. This AD requires 

revising the existing airplane flight 

manual (AFM) to incorporate a 

limitation and procedure for the wing 

anti-ice (WAI) system in order to 

mitigate the risk of ice accumulation on 

the wing leading edges. The FAA is 

issuing this AD to address the unsafe 

condition on these products. 

DATES: This AD is effective July 5, 2022. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of July 5, 2022. 

ADDRESSES: For service information 

identified in this final rule, contact 

Bombardier Business Aircraft Customer 

Response Center, 400 Coˆte-Vertu Road 

West, Dorval, Que ́bec H4S 1Y9, Canada; 

telephone 514–855–2999; email ac.yul@

aero.bombardier.com; internet 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. 

It is also available on the internet at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–0787. 

Examining the AD Docket 

You may examine the AD docket on 

the internet at https:// 

www.regulations.gov by searching for 

and locating Docket No. FAA–2021– 

0787; 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, 

any comments received, and other 

information. The address for Docket 

Operations is U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE, 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Chirayu Gupta, 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: 

Background 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

for Canada, has issued TCCA AD CF– 

2021–06, dated February 26, 2021 

(TCCA AD CF–2021–06) (also referred 

to after this as the Mandatory 

Continuing Airworthiness Information, 

or the MCAI), to correct an unsafe 

condition for certain Bombardier, Inc., 

Model CL–600–1A11 (600), CL–600– 

2A12 (601), and CL–600–2B16 (601–3A, 

601–3R, and 604 Variants) airplanes. 

You may examine the MCAI in the AD 

docket at https://www.regulations.gov 

by searching for and locating Docket No. 

FAA–2021–0787. 

The FAA issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain Bombardier, Inc., Model 

CL–600–1A11 (600), CL–600–2A12 

(601), and CL–600–2B16 (601–3A, 601– 

3R, and 604 Variants) airplanes. The 

NPRM published in the Federal 

Register on September 15, 2021 (86 FR 

51279). The NPRM was prompted by a 

report of a wing stall (wing drop/uncommanded roll) during a landing flare. 

The NPRM proposed to require revising 

the existing AFM to incorporate a 

limitation and procedure for the WAI 

system in order to mitigate the risk of 

ice accumulation on the wing leading 

edges. The FAA is issuing this AD to 

address ice accumulation on the wing 

leading edges, which could result in a 

wing stall during landing and 

consequent reduced controllability of 

the airplane. See the MCAI for 

additional background information. 

Comments 

The FAA gave the public the 

opportunity to participate in developing 

this final rule. The FAA received no 

comments on the NPRM or on the 

determination of the cost to the public. 

Conclusion 

The FAA reviewed the relevant data 

and determined that air safety and the 

public interest require adopting this 

final rule as proposed, except for minor 

editorial changes. 

The FAA has determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

addressing the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Related Service Information Under 1 

CFR Part 51 

Bombardier has issued the following 

service information, which specifies a 

revised AFM limitation and procedure 

for the WAI system in order to mitigate 

the risk of ice accumulation on the wing 

leading edge. These documents are 

distinct since they apply to different 

airplane configurations. 

• Sub-sub section (2), Wing Anti-ice 

System, of sub-section I., Operation in 

Icing Conditions, of Chapter 3., 

OPERATING LIMITATIONS, of the 

LIMITATIONS section of the Canadair 

Challenger AFM, Product Publication 

No. 600, Revision A114, dated April 16, 

2020. 

• Sub-section C., Icing Conditions 

During Flight, of Chapter 3., SYSTEMS 

OPERATIONS—ANTI-ICE, of the 

Canadair Challenger AFM, Product 

Publication No. 600, Revision A114, 

dated April 16, 2020. 


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