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PROPOSED AD THOMMEN AIRCRAFT EQUIPMENT AG: Docket No. FAA-2024-2322; Project Identifier MCAI-2024-00065-Q.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this  airworthiness directive (AD) by
    November 14, 2024.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

(1) This  AD applies  to  THOMMEN AIRCRAFT  EQUIPMENT  AG  (THOMMEN)  AC32
    Digital Air Data Computers (ADCs)  having an affected part as  defined
    in paragraph (f)(1) of this AD.

(2) This  appliance is  installed on,  but not  limited to,  the following
    aircraft models specified in Table  1 to paragraph (c)(2) of  this AD,
    certificated in any category.

          TABLE 1 TO PARAGRAPH (C)(2)--APPLICABLE AIRCRAFT MODELS
    ----------------------------------------------------------------------
        TYPE CERTIFICATE HOLDER                   AIRCRAFT MODEL          
    ----------------------------------------------------------------------
    Airbus Defense and Space S.A. (type    CN-235, CN-235-100, CN-235-200,
    certificate previously held by         and CN-235-300.
    Construcciones Aeronauticas, S.A.)...
    Airbus Helicopters...................  AS332C, AS332C1, AS332L,
                                           AS332L1, AS3323L2.
    Airbus Helicopters Deutschland GmbH    EC635T2+.
    (AHD).
    Bell Textron Inc.....................  212, 412, and 412EP.
    Bombardier Inc.......................  CL-600-1A11 (600).
    Columbia Helicopters Inc.............  234.
    General Atomics Aerotek Systems GmbHl  228-100, 228-101, 228-200, 228-
    (type certificate formerly held by     201, 228-202, and 228-212.
    DORNIER LUFTFAHRT Inc.).
    Gulfstream Aerospace LP..............  Westwind Astra 1124 (serial
                                           numbers 004-0410).
    International Air Response...........  C-130A.
    Leonardo S.p.a.......................  A109, A10A, A109A II, A109C,
                                           A109K2, A109S, 1099SP, and
                                           AW139.
    Textron Aviation Inc.................  200, 300, 500, 501, 550, and
                                            551.
    Viking Air Limited...................  CL-215-6B11 (CL-215T Variant).
    ----------------------------------------------------------------------

(3) This appliance is approved for installation and could be installed  on
    various aircraft modified by  Supplemental Type Certificate (STC)  No.
    SR09595RC or ST01523WI.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 3417, Air Data Computer.

(e) UNSAFE CONDITION

    This AD  was prompted  by occurrences  of AC32  Digital ADCs  stopping
    functioning due to the power module failing at temperatures below  -20
    degrees Celsius. The unsafe condition, if not addressed, could  result
    in  insufficient  navigational  data  provided  to  the  flight  crew,
    resulting in reduced control of the aircraft.

(f) DEFINITIONS

    For  the  purpose of  this  AD the  definitions  in paragraphs  (f)(1)
    through (4) of this AD apply:

(1) Affected  part:  THOMMEN   AC32  Digital  ADCs,  part  numbers   (P/N)
    AC32.10.21.10.XX,     AC32.10.21.11.XX,     AC32.11.21.10.XX,      and
    AC32.11.21.11.XX (where XX  represents any alpha/numerical  sequence),
    and  having a  serial number  (S/N) listed  in Appendix  A of  THOMMEN
    AIRCRAFT EQUIPMENT  Service Bulletin  SB AC32/07,  Revision 1.0, dated
    August 31, 2023 (THOMMEN SB AC32/07 Revision 1.0).

(2) Serviceable  part: Any  AC32.(X) Digital  ADC that  is not an affected
    part; or an affected part where the power module has been replaced  by
    THOMMEN, in  accordance with  the instructions  of THOMMEN  SB AC32/07
    Revision 1.0.

(3) Group 1 aircraft: Have an affected part installed.

(4) Group  2 aircraft:  Do not  have an  affected part  installed but  are
    eligible for AC32.(X) Digital ADC installation.

(g) COMPLIANCE

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

(h) REQUIRED ACTIONS

    For Group  1 aircraft:  Within 12  months after  the effective date of
    this AD, remove each affected part from service and replace it with  a
    serviceable   part  in   accordance  with   paragraph  3.A.   of   the
    Accomplishment Instructions in THOMMEN SB AC32/07 Revision 1.0, except
    where this material specifies to send the removed affected part to the
    manufacturer, this AD does not require that action.

(i) PARTS INSTALLATION PROHIBITION

    For Group 1 and  2 aircraft: As of  the effective date of  this AD, do
    not install an affected part on any aircraft.

(j) SPECIAL FLIGHT PERMITS

    A one-time special flight permit  may be issued in accordance  with 14
    CFR 21.197 and 21.199 in order to fly to a maintenance base to perform
    the required action  in this AD,  provided a flight  profile above -15
    degrees Celsius (5 degrees Fahrenheit) is maintained.

(k) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, 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 local Flight Standards District Office, as
    appropriate.  If  sending information  directly  to the  International
    Validation Branch, send it to  the attention of the person  identified
    in paragraph (l) of this  AD and email to: 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.

(l) ADDITIONAL INFORMATION

    For  more  information  about  this  AD,  contact  William Reisenauer,
    Aviation  Safety  Engineer,  FAA,  1600  Stewart  Avenue,  Suite  410,
    Westbury,  NY  11590;  phone:  (516)  228-7301;  email: 9-AVS-AIR-BACO
    -COS@faa.gov.

(m) MATERIAL INCORPORATED BY REFERENCE

(1) The  Director of  the Federal  Register approved  the incorporation by
    reference  (IBR) of  the material  listed in  this  paragraph  under 5
    U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this material as applicable to do the actions required by
    this AD, unless the AD specifies otherwise.

(i) THOMMEN AIRCRAFT EQUIPMENT Service Bulletin SB AC32/07, Revision  1.0,
    dated August 31, 2023.

(ii) [Reserved]

(3) For THOMMEN  AIRCRAFT EQUIPMENT material  in this AD,  contact THOMMEN
    AIRCRAFT EQUIPMENT AG, Hofackerstrasse 48, 4132 Muttenz,  Switzerland;
    phone:  +41  (0) 61  965  22 22;  email:  sales@thommen.aero; website:
    thommen.aero.

(4) You may view this material 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.

(5) You may view this material at the National Archives and Records Admin-
    istration (NARA). For information on the availability of this material
    at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations  or
    email fr.inspection@nara.gov.

Issued on September 24, 2024. Steven W. Thompson, Acting Deputy  Director,
Compliance & Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this NPRM by November 14, 2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-2322; Project Identifier MCAI-2024-00065-Q]
RIN 2120-AA64

Airworthiness Directives; THOMMEN AIRCRAFT EQUIPMENT AG Digital
Air Data Computers

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 THOMMEN AIRCRAFT EQUIPMENT AG (THOMMEN) AC32 Digital Air
Data Computers. This proposed AD results from occurrences of AC32
Digital Air Data Computers (ADCs) that stop functioning below certain
temperatures. This proposed AD would require replacing an affected AC32
Digital ADC with a serviceable part. The FAA is proposing this AD to
address the unsafe condition on these products.

DATES: The FAA must receive comments on this NPRM by November 14, 2024.

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-2024-2322; 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 THOMMEN AIRCRAFT EQUIPMENT material identified in this
proposed AD, contact THOMMEN AIRCRAFT EQUIPMENT AG, Hofackerstrasse 48,
4132 Muttenz, Switzerland; phone: +41 (0) 61 965 22 22; email:
sales@thommen.aero; website: thommen.aero.

You may view this material 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: William Reisenauer, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: (516) 228-7301; 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-2024-2322; Project Identifier
MCAI-2024-00065-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
William Reisenauer, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590. 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 2024-0024, dated January 24, 2024 (also referred to as the
MCAI), to correct an unsafe condition on certain THOMMEN AC32 Digital
ADCs. The MCAI states that there have been occurrences of certain AC32
Digital ADCs stopping functioning at temperatures below -20 degrees
Celsius. The error is detectable and does not transmit erroneous data.
The problem is caused by the power module and the affected units have
been identified. This condition, if not addressed, could result in
insufficient navigational data provided to the flight crew, resulting
in reduced control of the aircraft. The MCAI requires removing from
service each affected part and specifies that only serviceable parts as
defined in the MCAI may be installed.

You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-2322.

Material Incorporated by Reference Under 1 CFR Part 51


The FAA reviewed THOMMEN AIRCRAFT EQUIPMENT Service Bulletin SB
AC32/07, Revision 1.0, dated August 31, 2023 (THOMMEN SB AC32/07,
Revision 1.0). This material specifies procedures for determining if an
aircraft is equipped with an affected AC32 Digital ADC listed in
Appendix A, determining if the actions specified in THOMMEN SB AC32/07,
Revision 1.0, were already accomplished, and replacing any affected
THOMMEN AC32 Digital ADC.

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.

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 referenced above. The FAA is issuing this NPRM after
determining that the unsafe condition described previously is likely to
exist or develop on other products of the same type design.

Proposed AD Requirements in This NPRM


This proposed AD would require replacing affected AC32 Digital ADCs
with serviceable parts. This proposed AD would also prohibit the
installation of an affected AC32 Digital ADC on any aircraft.

Costs of Compliance


The FAA estimates that this AD, if adopted as proposed, would
affect 401 AC32 Digital ADCs that are installed on aircraft worldwide.
The FAA has no way of determining how many of these ADC are installed
on aircraft of U.S. registry.

The FAA estimates the following costs to comply with this proposed
AD. These costs assume all 401 AC32 Digital ADCs are installed on
aircraft of U.S. registry. The FAA expects a portion of the affected
population to exist outside of the U.S. and the estimated costs to be lower.

Estimated Costs

ACTION
LABOR COST
PARTS COST
COST PER PRODUCT
COST ON U.S. OPERATORS
Replace affected AC32 Digital ADC
12 work-hours x $85 per hour = $1,020.
$4,477
$5,497
$2,204,297

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected operators.

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: