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PROPOSED AD THALES AVS FRANCE SAS: Docket No. FAA-2023-1716; Project Identifier MCAI-2022-00168-Q.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    October 10, 2023.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD  applies  to  Thales AVS France SAS flight management computer
    navigation modules (FMC2 NAVM) part number (P/N) C13084CA03, installed
    on, but not limited to airplanes, certificated in any category.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 3400, Navigation System.

(e) UNSAFE CONDITION

    This AD was prompted by reports that, due to software issues,  certain
    FMC2 NAVM navigation modules provide erroneous data to the flight man-
    agement  computer,  compromising  safe flight  of  the  airplane. This
    condition, if not  addressed, could compromise  the safety margins  of
    the airplane and result in controlled flight into terrain.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIRED ACTIONS

(1) Within 30 days after the effective date of this AD, revise the Limita-
    tions Section of the existing airplane flight manual  (AFM)  for  your
    airplane by adding the information  in Table 1  to paragraph (g)(1) of
    this AD and Table 2 to paragraph (g)(1) of this AD.
    ______________________________________________________________________
        TABLE 1 TO PARAGRAPH (G)(1) - LIMITATIONS TO OPERATE THE FLIGHT   
                     MANAGEMENT SYSTEM (FMS) OF THE AIRPLANE              
                 [FORMULATED AS INSTRUCTIONS TO THE FLIGHT CREW]          
    ______________________________________________________________________
               LIMITATION NO.                 LIMITATION/INSTRUCTION
    ______________________________________________________________________
                    1                  For Procedure Turn, Tear Drop
                                        trajectory, specified turn
                                        direction or arc to fix leg in
                                        published navigation procedure,
                                        disengage FMS Navigation mode and
                                        engage Track mode with the
                                        expected Track target.

                    2                  When coupled to the AFCS, do not
                                        perform a Direct To while
                                        established in Turn.

                    3                  Do not revise the flight plan
                                        until GO AROUND safe altitude (as
                                        per Standard Operating Procedure)
                                        has been reached.

                    4                  Initialize the flight plan with at
                                        least an intermediate waypoint
                                        between departure and
                                        destination.

                    5                  Before flying a procedure
                                       (including associated missed
                                        approach) that requires to fly
                                        over a waypoint, check that the
                                        fly-over flag is displayed on
                                        MCDU FPLN page beside the
                                        constrained fix, as expected in
                                        the published chart. If the fly-
                                        over is missing, it shall be set
                                        manually.

                    6                  Do not use Vertical Step function.

                    7                  Do not activate the data save
                                        command.

                    8                  Do not use Offset function.
    ______________________________________________________________________

    ______________________________________________________________________
            TABLE 2 TO PARAGRAPH (G)(1) - FMS USER MANUAL LIMITATIONS     
    ______________________________________________________________________
               LIMITATION NO.                FMS USER MANUAL LIMITATIONS
    ______________________________________________________________________
                    1                      Operate the FMS respecting the
                                           limitations.

                    2                      Only operate the FMS of the
                                           airplane with a specifically
                                           trained crew, as defined in the
                                           FMS User Manual, for awareness
                                           and training on the mitigation
                                           means to recover from the issue
                                           "straight leg bypassing
                                           following arc to fix leg."
    ______________________________________________________________________

(i) Inserting a copy of this AD into the Limitations Section of the exist-
    ing AFM for your airplane  satisfies the requirement  of paragraph (g)
    (1) of this AD.

(ii) The actions required by paragraph (g)(1) of this AD  may be performed
     by the owner/operator (pilot)  holding at least  a private pilot cer-
     tificate  and  must be entered into the aircraft records showing com-
     pliance with this AD in accordance with 14 CFR 43.9(a)  and 91.417(a)
     (2)(v).  The record must be maintained as required  by 14 CFR 91.417,
     121.380, or 135.439.

(2) Within 30 days after the effective date  of this AD,  update the data-
    base for your Thales FMC2 NAVM,  P/N C13084CA03,  with a database that
    does not contain the procedures  specified  in  section II  of  Thales
    Service Information Letter F9111-J70859DN-00,  issued January 18, 2022
    (Thales SIL F9111-J70859DN-00).

(3) As of the effective date  of this AD,  do not install  a database  for
    your Thales FMC2 NAVM, P/N C13084CA03,  unless it does not include the
    procedures specified in section II of Thales SIL F9111-J70859DN-00.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager,  East Certification 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  branch,  send  it  to  the  attention  of  the   person
    identified in paragraph (i)(2) of this AD.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(i) ADDITIONAL INFORMATION

(1) Refer  to  European Union Aviation Safety Agency  (EASA) AD 2022-0024,
    dated February 4, 2022,  for related information.  This EASA AD may be
    found in the AD docket  at regulations.gov  under Docket No. FAA-2023-
    1716.

(2) For more information about this AD, contact Nicholas Rediess, Aviation
    Safety Engineer,  FAA,  1701 Columbia Avenue,  College Park, GA 30337;
    phone: (781) 238-7159; email: 9-AVS-AIR-BACO-COS@faa.gov.

(j) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference  (IBR)  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 the AD specifies otherwise.

(i) Thales Service Information Letter F9111-J70859DN-00 issued January 18,
    2022.

Note 1 to paragraph (j)(2)(i):  The footer on pages 2 through 32 of Thales
Service Information  Letter  F9111-J70859DN-00,  issued  January 18, 2022,
contains the text "Reference: 0026-F9111-J70859DN-00."

(ii) [Reserved]

(3) For  service  information  identified in this AD,  contact  Thales AVS
    France  SAS,  75-77 Avenue Marcel Dassault,  33700  Merignac,  France;
    phone: +33 7 86 33 59 20;  email: continued.airworthiness@thalesgroup.
    com.

(4) You may view this service information at the FAA,  Airworthiness Prod-
    ucts Section, Operational Safety Branch,  901 Locust,  Kansas City, MO
    64106. For information on the availability of this material at the FAA
    call (817) 222-5110.

(5) You may view  this service information  that is incorporated by refer-
    ence 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: www.archives.gov/federal-register/cfr/
    ibr-locations.html.

Issued on August 17, 2023.  Victor Wicklund, Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this NPRM by October 10, 2023.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1716; Project Identifier MCAI-2022-00168-Q]
RIN 2120-AA64

Airworthiness Directives; Thales AVS France SAS Flight Management
Computer Navigation Modules

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 Thales AVS France SAS (Thales) flight management computer
navigation modules (FMC2 NAVM) installed on, but not limited to,
airplanes. This AD was prompted by reports that, due to software
issues, certain FMC2 NAVM navigation modules provide erroneous data to
the flight management computer, compromising safe flight of the
airplane. This proposed AD would require revising the existing aircraft
flight manual (AFM) for your airplane and updating the navigation
database. This proposed AD would also prohibit installing a database
unless certain procedures were removed. The FAA is proposing this AD to
address the unsafe condition on these products.

DATES: The FAA must receive comments on this NPRM by October 10, 2023.

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 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.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1716; 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.
Material Incorporated by Reference:
For service information identified in this NPRM, contact
Thales AVS France SAS, 75-77 Avenue Marcel Dassault, 33700 Merignac,
France; phone: +33 7 86 33 59 20; email:
continued.airworthiness@thalesgroup.com.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 901 Locust,
Kansas City, MO 64106. For information on the availability of this
material at the FAA, call (817) 222-5110.

FOR FURTHER INFORMATION CONTACT: Nicholas Rediess, Aviation Safety
Engineer, FAA, 1701 Columbia Avenue, College Park, GA 30337; phone:
(781) 238-7159; email: 9-AVS-AIR-BACO-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-2023-1716; Project Identifier
MCAI-2022-00168-Q'' 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
this 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
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
Nicholas Rediess, Aviation Safety Engineer, FAA, 1701 Columbia Avenue,
College Park, GA 30337. Any commentary that the FAA receives which is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.

Background

The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2022-0024, dated February 4, 2022 (referred to after this as
``the MCAI''), to correct an unsafe condition for Thales FMC2 NAVM,
part number (P/N) C13084CA03, installed on, but not limited to Dassault
(formerly Br[eacute]guet) Br.1150 Atlantique 2 (ATL2) maritime patrol
airplanes. The MCAI states that Thales FMC2 NAVM, P/N C13084CA03,
provides erroneous guidance for navigation procedures of the flight
management system due to issues with the software. This condition, if
not addressed, could compromise the safety margins of the airplane. To
address the unsafe condition, the MCAI requires revising the AFM with
operational instructions for the affected airborne navigation
procedures of the AFM. The MCAI also requires updating the navigation
database software, and prohibits installing a database for the Thales
FMC2 NAVM, P/N C13084CA03, unless it does not include the procedures
specified in section II of Thales Service Information Letter F9111-
J70859DN-00, issued January 18, 2022 (Thales SIL F9111-J70859DN-00).
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1716.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Thales SIL F9111-J70859DN-00. This service
information specifies updating the Thales FMC2 NAVM, P/N C13084CA03,
navigation database.
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


These products have been approved by the aviation authority of
another country and are approved for operation in the United States.
Pursuant to the FAA's bilateral agreement with this State of Design
Authority, it has notified the FAA of the unsafe condition described in
the MCAI and service information referenced above. The FAA is issuing
this AD after determining the unsafe condition is likely to exist or
develop in other products of the same type design.

Proposed AD Requirements in This NPRM

This proposed AD would require revising the existing AFM for your
airplane and updating the navigation database. This proposed AD would
also prohibit installing a database for the Thales FMC2 NAVM, P/N
C13084CA03, unless it does not include the procedures specified in
section II of Thales SIL F9111-J70859DN-00.
The owner/operator (pilot) holding at least a private pilot
certificate may perform the proposed incorporation of the operating
limitation into the existing AFM of your airplane, and the actions must
be entered into the aircraft records showing compliance with this AD in
accordance with 14 CFR 43.9(a) and 91.417(a)(2)(v). The record must be
maintained as required by 14 CFR 91.417, 121.380, or 135.439. The
proposed incorporation of the operating limitation into the existing
AFM of your airplane is not considered a maintenance action and may be
done equally by a pilot or a mechanic. This is an exception to the
FAA's standard maintenance regulations.

Differences Between This Proposed AD and the MCAI

The MCAI applies to all Thales FMC2 NAVMs, P/N C13084CA03,
installed on, but not limited to Dassault (formerly Br[eacute]guet)
Br.1150 Atlantique 2 (ATL2) maritime patrol airplanes, and this
proposed AD would not apply to those airplanes because those airplanes
do not have an FAA type certificate. Currently, no airplanes on the
U.S. registry incorporate the navigation equipment affected by this AD.

Costs of Compliance


There are currently no affected airplanes on the U.S. registry with
a Thales FMC2 NAVM, P/N C13084CA03, installed. In the event a U.S.-
registered airplane would have this equipment installed, the following
is an estimate of the costs to comply with this proposed AD.

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Revise AFM and update navigation database 2 work-hours x $85 per hour = $170
$0
$170
$0

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.

Sec. 39.13 [Amended]


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