[Federal Register Volume 89, Number 2 (Wednesday, January 3, 2024)]
[Rules and Regulations]
[Pages 240-241]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-28852]



[[Page 240]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1896; Project Identifier MCAI-2023-00837-T; 
Amendment 39-22633; AD 2023-25-06]
RIN 2120-AA64


Airworthiness Directives; Saab AB, Support and Services (Formerly 
Known as Saab AB, Saab Aeronautics) Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Saab AB, Support and Services Model SAAB 2000 airplanes. This AD was 
prompted by a review of the anti-skid system that revealed the 
possibility of inadvertently connecting the inboard harness to the 
outboard channel (and vice versa) of the wheel speed transducers in the 
main landing gear (MLG) wheel axles. This AD requires installing color 
markings on the harnesses and the wheel axles, to ensure proper 
installation and connection of the anti-skid harnesses, as specified in 
a European Union Aviation Safety Agency (EASA) AD, which is 
incorporated by reference. The FAA is issuing this AD to address the 
unsafe condition on these products.

DATES: This AD is effective February 7, 2024.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of February 7, 
2024.

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-1896; 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.
    Material Incorporated by Reference:
    <bullet> For material incorporated by reference in this AD, contact 
EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone +49 221 
8999 000; email <a href="/cdn-cgi/l/email-protection#92d3d6e1d2f7f3e1f3bcf7e7e0fde2f3bcf7e7"><span class="__cf_email__" data-cfemail="2c6d685f6c494d5f4d0249595e435c4d024959">[email protected]</span></a>; website easa.europa.eu. You may 
find this material on the EASA website ad.easa.europa.eu.
    <bullet> You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th Street, 
Des Moines, WA. For information on the availability of this material at 
the FAA, call 206-231-3195. It is also available in the AD docket at 
regulations.gov under Docket No. FAA-2023-1896.

FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aviation Safety 
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
phone 206-231-3220; email <a href="/cdn-cgi/l/email-protection#5a29323b32283b37743e3b343f2932373b343e331a3c3b3b743d352c"><span class="__cf_email__" data-cfemail="daa9b2bbb2a8bbb7f4bebbb4bfa9b2b7bbb4beb39abcbbbbf4bdb5ac">[email protected]</span></a>.

SUPPLEMENTARY INFORMATION: 

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 by adding an AD that would apply to all Saab AB, Support 
and Services Model SAAB 2000 airplanes. The NPRM published in the 
Federal Register on October 5, 2023 (88 FR 69105). The NPRM was 
prompted by AD 2023-0135, dated July 10, 2023, issued by EASA, which is 
the Technical Agent for the Member States of the European Union (EASA 
AD 2023-0135) (also referred to as the MCAI). The MCAI states a system 
review of the anti-skid system revealed the possibility of 
inadvertently connecting the inboard harness to the outboard channel 
(and vice versa) of the wheel speed transducers in the MLG wheel axles. 
This condition, if not detected and corrected, would lead to wrong 
inputs to the anti-skid function, whenever activated, with consequent 
reduced braking capability, possibly resulting in damage to the 
airplane.
    In the NPRM, the FAA proposed to require modification of the MLG by 
installing color markings on the harnesses and the wheel axles, to 
ensure proper installation and connection of the anti-skid harnesses, 
as specified in EASA AD 2023-0135. The FAA is issuing this AD to 
address the unsafe condition on these products.
    You may examine the MCAI in the AD docket at regulations.gov under 
Docket No. FAA-2023-1896.

Discussion of Final Airworthiness Directive

Comments

    The FAA received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    This product has been approved by the aviation authority of another 
country and is 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 reviewed the relevant data and determined 
that air safety requires adopting this AD as proposed. Accordingly, the 
FAA is issuing this AD to address the unsafe condition on this product. 
Except for minor editorial changes, this AD is adopted as proposed in 
the NPRM. None of the changes will increase the economic burden on any 
operator.

Related Service Information Under 1 CFR Part 51

    EASA AD 2023-0135 specifies procedures for modifying the left- and 
right-hand MLG and connectors with color markings. 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.

Costs of Compliance

    The FAA estimates that this AD affects 17 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
10 work-hours x $85 per hour = $850..........................          $1,740           $2,590          $44,030
----------------------------------------------------------------------------------------------------------------


[[Page 241]]

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 that 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.

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

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:

2023-25-06 Saab AB, Support and Services (Formerly Known as Saab AB, 
Saab Aeronautics): Amendment 39-22633; Docket No. FAA-2023-1896; 
Project Identifier MCAI-2023-00837-T.

(a) Effective Date

    This airworthiness directive (AD) is effective February 7, 2024.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Saab AB, Support and Services (formerly 
known as Saab AB, Saab Aeronautics) Model SAAB 2000 airplanes, 
certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 32, Landing 
gear.

(e) Unsafe Condition

    This AD was prompted by a review of the anti-skid system that 
revealed the possibility of inadvertently connecting the inboard 
harness to the outboard channel (and vice versa) of the wheel speed 
transducers in the main landing gear (MLG) wheel axles. The FAA is 
issuing this AD to address incorrect connections of the harnesses to 
the wheel speed transducers. The unsafe condition, if not addressed, 
could result in wrong inputs to the anti-skid function, whenever 
activated, with consequent reduced braking capability, possibly 
resulting in damage to the airplane.

(f) Compliance

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

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, EASA AD 2023-0135, dated July 10, 2023 (EASA AD 
2023-0135).

(h) Exceptions to EASA AD 2023-0135

    (1) Where EASA AD 2023-0135 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) Where EASA AD 2023-0135 requires a ``visual check,'' this AD 
requires replacing those words with ``visual inspection.''
    (3) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0135.

(i) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): 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 responsible Flight Standards Office, as 
appropriate. If sending information directly to the manager of the 
International Validation Branch, mail it to the address identified 
in paragraph (j) of this AD or email to: <a href="/cdn-cgi/l/email-protection#497064081f1a6408001b647e7a79640804060a092f2828672e263f"><span class="__cf_email__" data-cfemail="b88195f9eeeb95f9f1ea958f8b8895f9f5f7fbf8ded9d996dfd7ce">[email protected]</span></a>. 
If mailing information, also submit information by email. Before 
using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
responsible Flight Standards Office.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain instructions from a manufacturer, the instructions must be 
accomplished using a method approved by the Manager, International 
Validation Branch, FAA; or EASA; or Saab AB, Support and Services' 
EASA Design Organization Approval (DOA). If approved by the DOA, the 
approval must include the DOA-authorized signature.

(j) Additional Information

    For more information about this AD, contact Shahram Daneshmandi, 
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; phone 206-231-3220; email 
<a href="/cdn-cgi/l/email-protection#d6a5beb7bea4b7bbf8b2b7b8b3a5bebbb7b8b2bf96b0b7b7f8b1b9a0"><span class="__cf_email__" data-cfemail="1f6c777e776d7e72317b7e717a6c77727e717b765f797e7e31787069">[email protected]</span></a>.

(k) 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 this AD specifies otherwise.
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0135, 
dated July 10, 2023.
    (ii) [Reserved]
    (3) For EASA AD 2023-0135, contact EASA, Konrad-Adenauer-Ufer 3, 
50668 Cologne, Germany; phone +49 221 8999 000; email 
<a href="/cdn-cgi/l/email-protection#7435300734111507155a1101061b04155a1101"><span class="__cf_email__" data-cfemail="0544417645606476642b6070776a75642b6070">[email protected]</span></a>; website easa.europa.eu. You may find this EASA 
AD on the EASA website ad.easa.europa.eu.
    (4) You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th 
Street, Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195.
    (5) You may view this material at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email <a href="/cdn-cgi/l/email-protection#cfa9bde1a6a1bcbfaaacbba6a0a18fa1aebdaee1a8a0b9"><span class="__cf_email__" data-cfemail="c9afbbe7a0a7bab9acaabda0a6a789a7a8bba8e7aea6bf">[email protected]</span></a>.

    Issued on December 14, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-28852 Filed 1-2-24; 8:45 am]
BILLING CODE 4910-13-P


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