Airworthiness Directives; Bombardier, Inc., Airplanes, 59739-59741 [2019-24192]

Download as PDF Federal Register / Vol. 84, No. 215 / Wednesday, November 6, 2019 / Proposed Rules List of Subjects in 7 CFR Part 932 Olives, Marketing agreements, Reporting and recordkeeping requirements. For the reasons set forth in the preamble, 7 CFR part 932 is proposed to be amended as follows: PART 932—OLIVES GROWN IN CALIFORNIA 1. The authority citation for 7 CFR part 932 continues to read as follows: ■ Authority: 7 U.S.C. 601–674. § 932.36 ■ [Amended] 2. Amend § 932.36 to read as follows: § 932.36 Procedure. Decisions of the committee shall be by majority vote of the members, including alternates acting as members, present and voting, and a quorum must be present: Provided, That decisions requiring a recommendation to the Secretary on matters pertaining to grade and size regulations shall require at least 10 affirmative votes, at least 5 of which must be from producer members and at least 5 of which must be from handler members and, if the committee is increased by the addition of a public member, at least 11 affirmative votes shall be required, at least 5 of which must be from producer members and at least 5 of which must be from handler members. A quorum shall consist of at least 10 members, including alternates acting as members, and, if the committee is increased by the addition of a public member, a quorum shall consist of at least 11 members, including alternates acting as members. Except in case of an emergency, a minimum of 5 days advance notice shall be given with respect to any meeting of the committee. In case of an emergency, to be determined within the discretion of the chairman of the committee, as much advance notice of a meeting as is practicable in the circumstances shall be given. The committee may vote by mail or telegram upon due notice to all members, but any proposition to be so voted upon first shall be explained accurately, fully, and identically by mail or telegram to all members. When voted on by such method, at least 14 affirmative votes, of which seven shall be producer member votes and seven shall be handler member votes, shall be required for adoption and, if the committee is increased by the addition of a public member, votes by mail or telegram shall require at least 15 affirmative votes, of which at least 7 shall be producer member votes and at least 7 shall be handler member votes. The committee may recommend for the VerDate Sep<11>2014 16:44 Nov 05, 2019 Jkt 250001 Secretary’s approval changes in the number of affirmative votes required for adoption of any proposition voted upon by means of a mail or telegram ballot: Provided, That the number of affirmative votes required for adoption shall not be less than ten, and in any case an equal number of producer member and handler member votes shall be required for adoption and, if the committee is increased by the addition of a public member, the number of affirmative votes required for adoption shall be increased by one. Dated: November 1, 2019. Bruce Summers, Administrator, Agricultural Marketing Service. [FR Doc. 2019–24224 Filed 11–5–19; 8:45 am] BILLING CODE 3410–02–P 59739 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., 200 Coˆte-Vertu Road West, Dorval, Que´bec H4S 2A3, Canada; North America toll-free phone: 1–866–538– 1247 or direct-dial phone: 1–514–855– 2999; email: ac.yul@aero.bombardier.com; internet: https://www.bombardier.com. You may view this service information at the FAA, Transport Standards 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 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2019–0728; Product Identifier 2019–NM–071–AD] RIN 2120–AA64 Airworthiness Directives; Bombardier, Inc., Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD– 100–1A10 airplanes. This proposed AD was prompted by a report that during ALTS CAP or (V) ALTS CAP mode, the flight guidance/autopilot does not account for engine failure while capturing an altitude. This proposed AD would require revising the existing airplane flight manual (AFM) to provide the flightcrew with new warnings for ‘‘Autoflight’’ and ‘‘Engine Failure in Climb During ALTS CAP.’’ 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 December 23, 2019. 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– SUMMARY: PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2019– 0728; 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 regulatory evaluation, any comments received, and other information. The street address for Docket Operations is listed above. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, Aerospace Engineer, Avionics and Electrical Systems Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516–228–7367; fax: 516– 794–5531; 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 the ADDRESSES section. Include ‘‘Docket No. FAA–2019–0728; Product Identifier 2019–NM–071–AD’’ at the beginning of your comments. The FAA specifically invites comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. The FAA will consider all comments received by the closing date and may amend this NPRM because of those comments. The FAA will post all comments received, without change, to https:// www.regulations.gov, including any personal information you provide. The E:\FR\FM\06NOP1.SGM 06NOP1 59740 Federal Register / Vol. 84, No. 215 / Wednesday, November 6, 2019 / Proposed Rules FAA will also post a report summarizing each substantive verbal contact received about this NPRM. Discussion Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian AD CF–2019–12, dated April 3, 2019 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for certain Bombardier, Inc., Model BD–100–1A10 airplanes. This proposed AD was prompted by a report that during ALTS CAP or (V) ALTS CAP mode, the flight guidance/ autopilot does not account for engine failure while capturing an altitude. The FAA is proposing this AD to address the occurrence of an engine failure during or before a climb while in ALTS CAP or (V) ALTS CAP mode, as it could cause the airspeed to drop significantly below the safe operating speed and may require prompt flightcrew intervention to maintain a safe operating speed. See the MCAI for more information. Related Service Information Under 1 CFR Part 51 Bombardier has issued the following service information, which provides new warnings for ‘‘Autoflight’’ and ‘‘Engine Failure in Climb During ALTS CAP,’’ in the LIMITATIONS—System Limitations and the EMERGENCY PROCEDURES—Powerplant sections of the applicable AFM. • Bombardier Challenger 300, Airplane Flight Manual, Publication No. CSP 100–1, Revision 55, dated April 8, 2019. • Bombardier Challenger 350, Airplane Flight Manual, Publication No. CH 350 AFM, Revision 21, dated April 8, 2019. These documents are distinct since they apply to different airplane models in different configurations. 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 a 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 agency 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 Requirements of This NPRM This proposed AD would require revising the existing AFM with new warnings for ‘‘Autoflight’’ and ‘‘Engine Failure in Climb During ALTS CAP,’’ in the LIMITATIONS—System Limitations and the EMERGENCY PROCEDURES— Powerplant sections, as described previously. Costs of Compliance The FAA estimates that this proposed AD affects 252 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 $21,420 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. This proposed AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is VerDate Sep<11>2014 16:44 Nov 05, 2019 Jkt 250001 normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes and associated appliances to the Director of the System Oversight Division. 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) 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 Frm 00005 Fmt 4702 List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Proposed Amendment Regulatory Findings PO 00000 under the criteria of the Regulatory Flexibility Act. Sfmt 4702 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. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ Bombardier, Inc.: Docket No. FAA–2019– 0728; Product Identifier 2019–NM–071– AD. E:\FR\FM\06NOP1.SGM 06NOP1 Federal Register / Vol. 84, No. 215 / Wednesday, November 6, 2019 / Proposed Rules (a) Comments Due Date The FAA must receive comments by December 23, 2019. (b) Affected ADs None. (c) Applicability This AD applies to Bombardier, Inc., Model BD–100–1A10 airplanes, certificated in any category, serial numbers 20003 through 20500 inclusive and 20501 through 20752 inclusive. (d) Subject Air Transport Association (ATA) of America Code 22, Auto flight. (e) Reason This AD was prompted by a report that during ALTS CAP or (V) ALTS CAP mode, the flight guidance/autopilot does not account for engine failure while capturing an altitude. The FAA is issuing this AD to address the occurrence of an engine failure during or before a climb while in ALTS CAP or (V) ALTS CAP mode, as it could cause the airspeed to drop significantly below the safe operating speed and may require prompt flightcrew intervention to maintain a safe operating speed. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Revision of the Airplane Flight Manual (AFM) Within 30 days after the effective date of this AD: Revise the LIMITATIONS—System Limitations and the EMERGENCY PROCEDURES—Powerplant sections of the existing AFM to include the information in ‘‘Autoflight’’ and ‘‘Engine Failure in Climb During ALTS CAP’’ of Bombardier Challenger 300, Airplane Flight Manual, Publication No. CSP 100–1, Revision 55, dated April 8, 2019 (for airplanes having serial numbers 20003 through 20500 inclusive); or Bombardier Challenger 350, Airplane Flight Manual, Publication No. CH 350 AFM, Revision 21, dated April 8, 2019 (for airplanes having serial numbers 20501 through 20752 inclusive). (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 local Flight Standards District 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; phone: 516– 228–7300; fax: 516–794–5531. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight VerDate Sep<11>2014 16:44 Nov 05, 2019 Jkt 250001 standards district office/certificate holding district office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action 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) Canadian AD CF–2019–12, dated April 3, 2019, 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–2019–0728. (2) For more information about this AD, contact Steven Dzierzynski, Aerospace Engineer, Avionics and Electrical Systems Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516–228–7367; fax: 516–794–5531; email: 9-avs-nyaco-cos@ faa.gov. (3) For service information identified in this AD, contact Bombardier, Inc., 200 CoˆteVertu Road West, Dorval, Que´bec H4S 2A3, Canada; North America toll-free phone: 1– 866–538–1247 or direct-dial phone: 1–514– 855–2999; email: ac.yul@ aero.bombardier.com; internet: https:// www.bombardier.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. Issued in Des Moines, Washington, on October 28, 2019. Dionne Palermo, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2019–24192 Filed 11–5–19; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF HOMELAND SECURITY Coast Guard 33 CFR Part 117 [Docket No. USCG–2018–0953] RIN 1625–AA09 Drawbridge Operation Regulations; Lacombe Bayou, LA Coast Guard, DHS. Notice of proposed rulemaking. AGENCY: ACTION: The Coast Guard proposes to change the operating schedule that governs the Tammany Trace swing bridge across Lacombe Bayou, mile 5.2, at Lacombe, St. Tammany Parish, Louisiana. This action is necessary to SUMMARY: PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 59741 effectively coordinate Tammany Trace trail operations and maintenance with drawbridge operations. DATES: Comments and related material must be received by the Coast Guard on or before December 6, 2019. ADDRESSES: You may submit comments identified by docket number USCG– 2018–0953 using Federal eRulemaking Portal at https://www.regulations.gov. See the ‘‘Public Participation and Request for Comments’’ portion of the SUPPLEMENTARY INFORMATION section for further instructions on submitting comments. If you have questions about this proposed rulemaking, call or email Mr. Doug Blakemore, Eighth Coast Guard District Bridge Administrator; telephone (504) 671–2128, email Douglas.A.Blakemore@ uscg.mil. SUPPLEMENTARY INFORMATION: FOR FURTHER INFORMATION CONTACT: I. Table of Abbreviations CFR Code of Federal Regulations DHS Department of Homeland Security FR Federal Register NPRM Notice of proposed rulemaking STP St. Tammany Parish Trace Tammany Trace § Section II. Background, Purpose and Legal Basis Saint Tammany Parish (STP) has requested to change the operating requirements for the Tammany Trace swing bridge across Lacombe Bayou, mile 5.2, at Lacombe, St. Tammany Parish, Louisiana. This bridge currently opens on signal according to 33 CFR 117.5. STP has requested to open the bridge if vessels provide 2 hours advance notification. This bridge spans the Tammany Trace which is a park area that is used by pedestrians and bicyclists. The Trace is open from 7 a.m. to 7:30 p.m. daily. The bridge operates during Trace hours and is secured in the open to navigation position when the Trace is closed. This bridge has a vertical clearance of 9.7 feet above mean high water in the closed to vessel position and unlimited vertical clearance in the open to vessel traffic position. There are few vessel movements through this bridge. From 2015 through 2017 the bridge opened 197 times for vessel passage. This waterway is primarily used by recreational boaters in the Lacombe area and does not support commercial activity. In addition to bridge operations, STP bridge tenders assist with Trace bike, pedestrian and equestrian operations and maintenance. This change would E:\FR\FM\06NOP1.SGM 06NOP1

Agencies

[Federal Register Volume 84, Number 215 (Wednesday, November 6, 2019)]
[Proposed Rules]
[Pages 59739-59741]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-24192]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0728; Product Identifier 2019-NM-071-AD]
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-100-1A10 airplanes. This 
proposed AD was prompted by a report that during ALTS CAP or (V) ALTS 
CAP mode, the flight guidance/autopilot does not account for engine 
failure while capturing an altitude. This proposed AD would require 
revising the existing airplane flight manual (AFM) to provide the 
flightcrew with new warnings for ``Autoflight'' and ``Engine Failure in 
Climb During ALTS CAP.'' 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 December 
23, 2019.

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., 200 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec 
H4S 2A3, Canada; North America toll-free phone: 1-866-538-1247 or 
direct-dial phone: 1-514-855-2999; email: [email protected]; 
internet: https://www.bombardier.com. You may view this service 
information at the FAA, Transport Standards 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0728; 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 regulatory evaluation, any comments received, and other 
information. The street address for Docket Operations is listed above. 
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, Aerospace 
Engineer, Avionics and Electrical Systems Services Section, FAA, New 
York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
phone: 516-228-7367; fax: 516-794-5531; 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 the ADDRESSES section. Include ``Docket No. FAA-2019-0728; 
Product Identifier 2019-NM-071-AD'' at the beginning of your comments. 
The FAA specifically invites comments on the overall regulatory, 
economic, environmental, and energy aspects of this NPRM. The FAA will 
consider all comments received by the closing date and may amend this 
NPRM because of those comments.
    The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide. 
The

[[Page 59740]]

FAA will also post a report summarizing each substantive verbal contact 
received about this NPRM.

Discussion

    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian AD CF-2019-12, dated April 3, 
2019 (referred to after this as the Mandatory Continuing Airworthiness 
Information, or ``the MCAI''), to correct an unsafe condition for 
certain Bombardier, Inc., Model BD-100-1A10 airplanes.
    This proposed AD was prompted by a report that during ALTS CAP or 
(V) ALTS CAP mode, the flight guidance/autopilot does not account for 
engine failure while capturing an altitude. The FAA is proposing this 
AD to address the occurrence of an engine failure during or before a 
climb while in ALTS CAP or (V) ALTS CAP mode, as it could cause the 
airspeed to drop significantly below the safe operating speed and may 
require prompt flightcrew intervention to maintain a safe operating 
speed. See the MCAI for more information.

Related Service Information Under 1 CFR Part 51

    Bombardier has issued the following service information, which 
provides new warnings for ``Autoflight'' and ``Engine Failure in Climb 
During ALTS CAP,'' in the LIMITATIONS--System Limitations and the 
EMERGENCY PROCEDURES--Powerplant sections of the applicable AFM.
     Bombardier Challenger 300, Airplane Flight Manual, 
Publication No. CSP 100-1, Revision 55, dated April 8, 2019.
     Bombardier Challenger 350, Airplane Flight Manual, 
Publication No. CH 350 AFM, Revision 21, dated April 8, 2019.
    These documents are distinct since they apply to different airplane 
models in different configurations. 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 a 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 agency 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 Requirements of This NPRM

    This proposed AD would require revising the existing AFM with new 
warnings for ``Autoflight'' and ``Engine Failure in Climb During ALTS 
CAP,'' in the LIMITATIONS--System Limitations and the EMERGENCY 
PROCEDURES--Powerplant sections, as described previously.

Costs of Compliance

    The FAA estimates that this proposed AD affects 252 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          $21,420
----------------------------------------------------------------------------------------------------------------

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.
    This proposed AD is issued in accordance with authority delegated 
by the Executive Director, Aircraft Certification Service, as 
authorized by FAA Order 8000.51C. In accordance with that order, 
issuance of ADs is normally a function of the Compliance and 
Airworthiness Division, but during this transition period, the 
Executive Director has delegated the authority to issue ADs applicable 
to transport category airplanes and associated appliances to the 
Director of the System Oversight Division.

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) 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 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.


Sec.  39.13  [Amended]

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

Bombardier, Inc.: Docket No. FAA-2019-0728; Product Identifier 2019-
NM-071-AD.

[[Page 59741]]

(a) Comments Due Date

    The FAA must receive comments by December 23, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Bombardier, Inc., Model BD-100-1A10 
airplanes, certificated in any category, serial numbers 20003 
through 20500 inclusive and 20501 through 20752 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Code 22, Auto flight.

(e) Reason

    This AD was prompted by a report that during ALTS CAP or (V) 
ALTS CAP mode, the flight guidance/autopilot does not account for 
engine failure while capturing an altitude. The FAA is issuing this 
AD to address the occurrence of an engine failure during or before a 
climb while in ALTS CAP or (V) ALTS CAP mode, as it could cause the 
airspeed to drop significantly below the safe operating speed and 
may require prompt flightcrew intervention to maintain a safe 
operating speed.

(f) Compliance

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

(g) Revision of the Airplane Flight Manual (AFM)

    Within 30 days after the effective date of this AD: Revise the 
LIMITATIONS--System Limitations and the EMERGENCY PROCEDURES--
Powerplant sections of the existing AFM to include the information 
in ``Autoflight'' and ``Engine Failure in Climb During ALTS CAP'' of 
Bombardier Challenger 300, Airplane Flight Manual, Publication No. 
CSP 100-1, Revision 55, dated April 8, 2019 (for airplanes having 
serial numbers 20003 through 20500 inclusive); or Bombardier 
Challenger 350, Airplane Flight Manual, Publication No. CH 350 AFM, 
Revision 21, dated April 8, 2019 (for airplanes having serial 
numbers 20501 through 20752 inclusive).

(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 local Flight Standards District 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; phone: 516-228-7300; fax: 516-794-5531. Before 
using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
local flight standards district office/certificate holding district 
office.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action 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) Canadian AD CF-2019-12, dated April 3, 2019, 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-2019-0728.
    (2) For more information about this AD, contact Steven 
Dzierzynski, Aerospace Engineer, Avionics and Electrical Systems 
Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, 
Suite 410, Westbury, NY 11590; phone: 516-228-7367; fax: 516-794-
5531; email: [email protected].
    (3) For service information identified in this AD, contact 
Bombardier, Inc., 200 C[ocirc]te-Vertu Road West, Dorval, 
Qu[eacute]bec H4S 2A3, Canada; North America toll-free phone: 1-866-
538-1247 or direct-dial phone: 1-514-855-2999; email: 
[email protected]; internet: https://www.bombardier.com. 
You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.

    Issued in Des Moines, Washington, on October 28, 2019.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2019-24192 Filed 11-5-19; 8:45 am]
BILLING CODE 4910-13-P
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.