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2020-08-02 THALES AVS FRANCE SAS: Amendment 39-21108; Docket No. FAA-2019-0760; Project Identifier 2019-NE-18-AD.
(a) EFFECTIVE DATE

    This AD is effective May 19, 2020.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Thales  AVS France SAS (Thales) Global  Positioning
    System/Satellite  Based  Augmentation  System  (GPS/SBAS)   receivers,
    Topstar 200 LPV, part numbers (P/Ns) C17149JA02 and C17149HA01.  These
    GPS/SBAS  receivers  are installed  on,  but not  limited  to, ATR-GIE
    Avions de Transport Regional (ATR) model ATR42 and ATR72 airplanes and
    Sikorsky Aircraft Corporation model S-76D helicopters, respectively.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 3457,  Global  Positioning
    System.

(e) UNSAFE CONDITION

    This AD was prompted  by  reports  that Thales GPS/SBAS receivers pro-
    vided,  under  certain  conditions,  erroneous  outputs  on   aircraft
    positions. The FAA  is issuing this  AD to prevent  erroneous aircraft
    position  outputs  from  the  Thales  GPS/SBAS  receivers.  The unsafe
    condition, if not  addressed, could result  in controlled flight  into
    terrain and loss of the aircraft.

(f) COMPLIANCE

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

(g) REQUIRED ACTIONS

(1) For operators of affected ATR model ATR42 and ATR72 airplanes:

(i) Update the aircraft's navigation database  within  30  days  after the
    effective date of this AD  using the software upload instructions,  as
    applicable, in the following:

(A) ATR72 Aircraft Maintenance Manual (AMM)  Job  Instruction  Cards, Doc.
    No. 45-11-00 LDG 10030-004, dated June 1, 2018.

(B) ATR42-400/500 Series AMM Job Instruction Cards,  Doc. No. 45-11-00 LDG
    10030-004, dated July 1, 2018.

(C) Thales Service Information Letter (SIL) Doc. No. THAV/SIL-1308,  Issue
    7, dated September 28, 2018.

(ii) [Reserved]

(2) For operators of affected ATR model ATR42 and ATR72 airplanes:

(i) Within 30 days after the effective date of this AD,  amend Section 1.2
    "Each Flight Checks" of the pre-flight section  in the applicable air-
    plane flight manual  by  inserting  the  change  shown in Figure 1 and
    Figure 2 to paragraph (g)(2)(i) of this AD.

    ______________________________________________________________________
    FIGURE 1 TO PARAGRAPH (G)(2)(I) –RESET INSTRUCTIONS FOR 1 GPS RECEIVER
                                     INSTALLED                            
    ______________________________________________________________________
         - DATA/INIT/POS INIT page ........................ DISPLAY
         - GPS POS key .................................... SELECT
         - C/B NAV/COM/SURV GPS 1 ......................... PULL
         - After 10 s
             - C/B NAV/COM/SURV GPS 1 ..................... PUSH
             - SENSOR INIT-key ............................ SELECT
    ______________________________________________________________________

    ______________________________________________________________________
    FIGURE 2 TO PARAGRAPH (G)(2)(I)–RESET INSTRUCTIONS FOR 2 GPS RECEIVERS
                                    INSTALLED                             
    ______________________________________________________________________
         - DATA/INIT/POS INIT page ........................ DISPLAY
         - GPS POS key .................................... SELECT
         - C/B NAV/COM/SURV GPS 1 ......................... PULL
         - C/B NAV/COM/SURV GPS 2 ......................... PULL
         - After 10 s
             - C/B NAV/COM/SURV GPS 1 ..................... PUSH
             - C/B NAV/COM/SURV GPS 2 ..................... PUSH
             - SENSOR INIT-key ............................ SELECT
    ______________________________________________________________________

(ii) Before each flight, power cycle the Thales GPS/SBAS receiver unit.

(3) For operators of Sikorsky S-76D helicopters,  within 30 days after the
    effective date of this AD,  update  the aircraft's navigation database
    using  the  instructions  in  TASK 31-61-00-800-802, "2.  FMS Database
    Update  for  Multifunction  Display  (MFD)"  of  the Sikorsky Aircraft
    Corporation, AMM SA S76D-AMM-000, 31-61-00, dated November 30, 2017.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager,  Boston  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
    Boston ACO Branch, send it  to the attention of the  person identified
    in paragraph (i)(1) 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) RELATED INFORMATION

(1) For more information about this AD,  contact Kirk Gustafson, Aerospace
    Engineer, Boston ACO Branch, FAA, 1200 District Avenue, Burlington, MA
    01803;  phone: 781-238-7190; fax: 781-238-7199; email: kirk.gustafson@
    faa.gov.

(2) Refer  to  European Union Aviation Safety Agency (EASA)  AD 2019-0004,
    dated January 11, 2019  (corrected on January 17, 2019),  for more in-
    formation.  You may examine the EASA AD in the AD docket on the inter-
    net  at  https://www.regulations.gov  by  searching  for  and locating
    Docket No. FAA-2019-0760.

(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) Sikorsky Aircraft Corporation,  Aircraft  Maintenance  Manual (AMM) SA
    S76D-AMM-000, 31-61-00, dated November 30, 2017.

(ii) ATR72 AMM  Job  Instruction  Cards,  Doc. No. 45-11-00 LDG 10030-004,
     dated June 1, 2018.

(iii) ATR42-400/500  Series  AMM Job Instruction Cards,  Doc. No. 45-11-00
      LDG 10030-004, dated July 1, 2018.

(iv) Thales Service Information Letter  Doc. No. THAV/SIL-1308,  Issue  7,
     dated September 28, 2018.

(3) For Sikorsky Aircraft Corporation  service information  identified  in
    this AD,  contact  Sikorsky  Aircraft  Corporation,  Customer  Service
    Engineering,  124 Quarry Road,  Trumbull, CT 06611;  telephone  1-800-
    Winged-S or 203-416-4299; email: wcs_cust_service_eng.gr-sik@lmco.com.

(4) For Thales service information identified in this AD,  contact  Thales
    AVS France SAS,  75-77 Avenue Marcel Dassault,  33700 Merignac-France,
    Tel: +33 (0)5 24 44 77 40, www.thalesgroup.com.

(5) For ATR service information identified  in  this  AD,  contact ATR-GIE
    Avions de Transport Regional,  1,  Allee Pierre Nadot,  31712  Blagnac
    Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33 (0) 5 62 21 67
    18; email continued.airworthiness@atr-aircraft.com.

(6) You may view  this  service  information  at  FAA,  Engine & Propeller
    Standards Branch,  1200 District Avenue, Burlington, MA 01803. For in-
    formation on the availability of this material  at the FAA,  call 781-
    238-7759.

(7) You  may  view  this  service  information  that  is  incorporated  by
    reference at the National Archives and Records Administration  (NARA).
    For information on the availability of this material  at  NARA, email:
    fedreg.legal@nara.gov,  or  go  to:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued on April 8, 2020. Ross Landes, Deputy Director for Regulatory Oper-
ations,  Compliance  &  Airworthiness  Division,   Aircraft  Certification
Service.

FOR FURTHER INFORMATION CONTACT:Kirk Gustafson, Aerospace Engineer, Boston
ACO Branch, FAA, 1200 District Avenue, Burlington, MA, 01803;  phone: 781-
238-7190; fax: 781-238-7199; email: kirk.gustafson@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0760; Project Identifier 2019-NE-18-AD; Amendment
39-21108; AD 2020-08-02]
RIN 2120-AA64

Airworthiness Directives; Thales AVS France SAS Global
Positioning System/Satellite Based Augmentation System Receivers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Thales AVS France SAS (Thales) Global Positioning System/
Satellite Based Augmentation System (GPS/SBAS) receivers installed on
airplanes and helicopters. This AD was prompted by reports that Thales
GPS/SBAS receivers provided, under certain conditions, erroneous
outputs on aircraft positions. This AD requires the installation of a
software update to the aircraft navigation database and insertion of a
change to the applicable airplane flight manual (AFM). The FAA is
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective May 19, 2020.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of May 19, 2020.

ADDRESSES: For service information identified in this final rule,
contact Sikorsky Aircraft Corporation, Customer Service Engineering,
124 Quarry Road, Trumbull, CT 06611; telephone 1-800-Winged-S or 203-
416-4299; email: wcs_cust_service_eng.gr-sik@lmco.com; Thales AVS
France SAS, 75-77 Avenue Marcel Dassault, 33700 Merignac--
France, Tel: +33 (0)5 24 44 77 40, www.thalesgroup.com; or ATR-GIE
Avions de Transport Regional, 1, Allee Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33
(0) 5 62 21 67 18; email continued.airworthiness@atr-aircraft.com. You may
view this service information at the FAA, Engine and Propeller Standards Branch,
1200 District Avenue, Burlington, MA, 01803. For information on the
availability of this material at the FAA, call 781-238-7759. It is also
available on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2019-0760.

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-
0760; 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: Kirk Gustafson, Aerospace Engineer,
Boston ACO Branch, FAA, 1200 District Avenue, Burlington, MA, 01803;
phone: 781-238-7190; fax: 781-238-7199; email: kirk.gustafson@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Thales GPS/SBAS
receivers installed on airplanes and helicopters. The NPRM published in
the Federal Register on January 31, 2020 (85 FR 5584). The NPRM was
prompted by reports that Thales GPS/SBAS receivers provided, under
certain conditions, erroneous outputs on aircraft positions. The NPRM
proposed to require the installation of a software update to the
aircraft navigation database and insertion of a change to the
applicable AFM. The FAA is issuing this AD to address the unsafe
condition on these products.
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Community, has
issued EASA AD 2019-0004, dated January 11, 2019, corrected on January
17, 2019 (referred to after this as ``the MCAI''), to address the
unsafe condition on these products. The MCAI states:

It has been determined that, in SBAS areas, in specific
conditions of the GPS satellite constellation in line of sight to
the aircraft, the Thales Topstar 200 LPV GPS/SBAS receiver may
provide an erroneous position on its outputs, which may not be
detected by the integrity check. Depending on the aircraft
installation, this error may not be noticed by the flight crew.
This condition, if not corrected, could possibly compromise the
safety margins when the receiver is used for Localizer Performance
with Vertical guidance (LPV) and/or RNP-AR (Required Navigation
Performance--Authorization Required) operations.
For the reasons described above, this [EASA] AD requires removal
from the navigation database of LPV procedures and all RNP-AR
procedures in SBAS areas, listed in the SIL. To ensure a reset of
all the GPS computations which may contribute to the erroneous GPS
position output, this [EASA] AD also requires, for certain ATR
aeroplanes (see Note 1 of this [EASA] AD), amendment of the
applicable AFM.

You may obtain further information by examining the MCAI in the AD
docket on the internet at https://www.regulations.gov by searching for
and locating Docket No. FAA-2019-0760.

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.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Task 31-61-00-800-802, ``2. FMS Database Update
for Multifunction Display (MFD)'' of the Sikorsky Aircraft Corporation,
Aircraft Maintenance Manual (AMM) SA S76D-AMM-000, 31-61-00, dated
November 30, 2017. This Task provides instructions for updating the MFD
on affected Sikorsky aircraft.
The FAA also reviewed ATR72 AMM Job Instruction Cards, Doc. No. 45-
11-00 LDG 10030-004, dated June 1, 2018, and ATR42-400/500 Series AMM
Job Instruction Cards, Doc. No. 45-11-00 LDG 10030-004, dated July 1,
2018. These service documents provide instructions on updating the
navigation databases installed on affected ATR airplanes.
The FAA also reviewed Thales Service Information Letter (SIL) Doc.
No. THAV/SIL-1308, Issue 7, dated September 28, 2018. The SIL describes
procedures to upload navigational database using Thales PMAT software
on affected ATR airplanes.
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.

Costs of Compliance

The FAA estimates that this AD affects 45 Thales GPS/SBAS receivers
installed on, but not limited to, GIE Avions de Transport
Regional model ATR42 airplanes and Sikorsky Aircraft Corporation
model S-76D helicopters of U.S. registry.
The FAA estimates the following costs to comply with this AD:

Estimated Costs

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Update navigation database for GPS/SBAS receiver. 1 work-hour x $85 per hour = $85
$0
$85
$3,825
Update AFM 3 work-hours x $85 per hour = $255
0
255
11,475

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 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.

Adoption of 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.

Sec. 39.13 [Amended]

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