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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2019-0582; Product Identifier 2019-NM-034-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by September 26, 2019.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to Bombardier, Inc.,  airplanes, certificated in  any
    category, identified in paragraphs (c)(1) through (c)(3) of this AD.

(1) Model CL-600-1A11 (600), serial numbers 1001 through 1085 inclusive.

(2) Model CL-600-2A12 (601), serial numbers 3001 through 3066 inclusive.

(3) Model CL-600-2B16  (601-3A and 601-3R  Variants), serial numbers  5001
    through 5194 inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 34, Navigation.

(e) REASON

    This AD was  prompted by reports  of the loss  of all air  data system
    information provided to the flightcrew,  which was caused by icing  at
    high altitudes. The FAA is issuing this AD to address the loss of  all
    air  data  system  information  provided  to  the  flightcrew.  If not
    addressed, this condition may  adversely affect continued safe  flight
    and landing.

(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
    Emergency  Procedures  section  of the  existing  AFM  to include  the
    information in the "Unreliable  Airspeed" procedure of the  applicable
    AFM specified in figure 1 to paragraph (g) of this AD.

AIRPLANE SERIAL NUMBERS

AFM

AFM REVISION

ISSUE DATE

CL-600-lAll (600) serial numbers 1001 through 1085 inclusive for non-winglets

Canadair Challenger CL-600-1A11 AFM, Product Publication (PP) 600

Revision A111

August 31, 2018

CL-600-lAll (600) serial numbers 1001 through 1085 inclusive for winglets

Canadair Challenger CL-600-1A11 (Winglets) AFM, Product Support Publication (PSP) 600-1

Revision 103

August 31, 2018

CL-600-2Al2 (601) serial numbers 3001 through 3066 inclusive

Canadair Challenger CL-600-2Al2 AFM,PSP 601-1A

Revision 120

August 31, 2018

CL-600-2Al2 (601) serial numbers 3001 through 3066 inclusive with Bombardier Service Bulletin 601-0360 incorporated

Canadair Challenger CL-600-2Al2 AFM,PSP 601-1A-1

Revision 79

August 31, 2018

CL-600-2Al2 (601) serial numbers 3001 through 3066 inclusive with -3A engine

Canadair Challenger CL-600-2Al2 AFM,PSP 601-1B

Revision 83

August 31, 2018

CL-600-2Al2 (601) serial numbers 3001 through 3066 inclusive with -3A engine and Bombardier Service Bulletin 601-0360 incorporated

Canadair Challenger CL-600-2Al2 AFM,PSP 601-1B-1

Revision 81

August 31, 2018

CL-600-2Bl6 (601-3A and 601-3R Variants) serial numbers 5001 through 5194 inclusive

Canadair Challenger CL-600-2B 16 AFM,PSP 601A-l

Revision 103

August 31, 2018

CL-600-2Bl6 (601-3A and 601-3R Variants) serial numbers 5001 through 5194 inclusive with Bombardier Service Bulletin 601-0360 incorporated

Canadair Challenger CL-600-2B 16 AFM,PSP 601A-l-1

Revision 92

August 31, 2018

    FIGURE 1 TO PARAGRAPH (G)  AFM REVISIONS

(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;
    telephone 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-2018-36,  dated   December  27,  2018,  for   related
    information. This MCAI may be found  in the AD docket on the  internet
    at http://www.regulations.gov by searching for and locating Docket No.
    FAA-2019-0582.

(2) For  more information  about this  AD, contact  John DeLuca, Aerospace
    Engineer, Avionics and Electrical  Systems Services Section, FAA,  New
    York ACO Branch, 1600 Stewart  Avenue, Suite 410, Westbury, NY  11590;
    telephone   516-228-7369;   fax   516-794-5531;   email    9-avs-nyaco
    -cos@faa.gov.

(3) For  service information  identified in  this AD,  contact Bombardier,
    Inc., 200 C[ocirc]te-Vertu Road West, Dorval, Quebec H4S 2A3,  Canada;
    North  America  toll-free  telephone  1-866-538-1247  or   direct-dial
    telephone 1-514-855-2999;  email ac.yul@aero.bombardier.com;  internet
    http://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 July 26, 2019. Dionne Palermo, Acting
Director, System Oversight Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD by  September 26,
2019.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2019-0582; Product Identifier 2019-NM-034-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 CL-600-1A11 (600), CL-600-2A12
(601), and CL-600-2B16 (601-3A and 601-3R Variants) airplanes. This
proposed AD was prompted by reports of the loss of all air data system
information provided to the flightcrew, which was caused by icing at
high altitudes. This proposed AD would require revising the exisitng
airplane flight manual (AFM) to provide the flightcrew with procedures
for "Unreliable Airspeed" that stabilize the airplane's airspeed and
attitude. 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 September
26, 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 http://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 telephone 1-866-538-1247 or
direct-dial telephone 1-514-855-2999; email ac.yul@aero.bombardier.com;
internet http://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 http://www.regulations.gov
by searching for and locating Docket No. FAA-2019-
0582; 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: John DeLuca, Aerospace Engineer,
Avionics and Electrical Systems Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7369; 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-2019-0582;
Product Identifier 2019-NM-034-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
http://www.regulations.gov, including any personal information you provide.
The 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-2018-36, dated December
27, 2018 (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 and 601-3R Variants) airplanes.
The MCAI states:

A number of in-service incidents have been reported on CL-600-
2C10 aeroplanes regarding the loss of all air data system
information provided to the crew. The air data system information
was recovered as the aeroplanes descended to lower altitudes. An
investigation determined that the root cause in both events was high
altitude icing (ice crystal contamination). If not recognized and
addressed, this condition may affect continued safe flight and landing.

Due to similarities in the air data systems, similar events
could also occur on Bombardier Inc. CL-600-1A11, CL-600-2A12 and CL-
600-2B16 aeroplanes.

This [Canadian] AD mandates the incorporation of Airplane Flight
Manual (AFM) procedures that will allow the crew to stabilize the
aeroplane's airspeed and attitude for continued safe flight and
landing.

You may examine the MCAI in the AD docket on the internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2019-0582.

Related Service Information Under 1 CFR Part 51


Bombardier has issued the following service information, which
provides a procedure for "Unreliable Airspeed" in the Emergency
Procedures section of the applicable AFM.

Canadair Challenger CL-600-1A11 AFM, Product Publication
(PP) 600, Revision A111, dated August 31, 2018.

Canadair Challenger CL-600-1A11 (Winglets) AFM, Product
Support Publication (PSP) 600-1, Revision 103, dated August 31, 2018.

Canadair Challenger CL-600-2A12 AFM, PSP 601-1A, Revision
120, dated August 31, 2018.

Canadair Challenger CL-600-2A12 AFM, PSP 601-1A-1,
Revision 79, dated August 31, 2018.

Canadair Challenger CL-600-2A12 AFM, PSP 601-1B, Revision
83, dated August 31, 2018.

Canadair Challenger CL-600-2A12 AFM, PSP 601-1B-1,
Revision 81, dated August 31, 2018.

Canadair Challenger CL-600-2B16 AFM, PSP 601A-1, Revision
103, dated August 31, 2018.

Canadair Challenger CL-600-2B16 AFM, PSP 601A-1-1,
Revision 92, dated August 31, 2018.

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
procedures for "Unreliable Airspeed" in the Emergency Procedures
section of the applicable AFM as described previously.

Costs of Compliance


The FAA estimates that this proposed AD affects 206 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 x $85 per hour = $85
$0
$85
$17,510

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


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]


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