[Federal Register Volume 82, Number 213 (Monday, November 6, 2017)]
[Rules and Regulations]
[Pages 51340-51342]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-23344]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0777; Product Identifier 2017-NM-050-AD; Amendment 
39-19089; AD 2017-22-09]
RIN 2120-AA64


Airworthiness Directives; Saab AB, Saab Aeronautics (Formerly 
Known as Saab AB, Saab Aerosystems) Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Saab AB, Saab Aeronautics Model SAAB 340B airplanes. This AD was 
prompted by reports of natural stall events in icing conditions, 
without prior stall warnings. This AD requires modifying the stall 
warning system, installing new stall warning computers, and activating 
the stall warning system. We are issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective December 11, 2017.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of December 11, 
2017.

ADDRESSES: For service information identified in this final rule, 
contact Saab AB, Saab Aeronautics, SE-581 88, Link[ouml]ping, Sweden; 
telephone +46 13 18 5591; fax +46 13 18 4874; email 
<a href="/cdn-cgi/l/email-protection#0e7d6f6f6c3d3a3e7a6b6d667d7b7e7e617c7a4e7d6f6f6c697c617b7e206d6163"><span class="__cf_email__" data-cfemail="becddfdfdc8d8a8ecadbddd6cdcbceced1cccafecddfdfdcd9ccd1cbce90ddd1d3">[email protected]</span></a>; Internet http://www.saabgroup.com. 
You may view this referenced service

[[Page 51341]]

information at the FAA, Transport Standards Branch, 1601 Lind Avenue 
SW., Renton, WA. For information on the availability of this material 
at the FAA, call 425-227-1221. It is also available on the Internet at 
http://www.regulations.gov by searching for and locating Docket No. 
FAA-2017-0777.

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-2017-
0777; or in person at the Docket Management Facility between 9 a.m. and 
5 p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this AD, the regulatory evaluation, any comments received, and 
other information. The street address for the Docket Office (telephone 
800-647-5527) is Docket Management Facility, 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: Shahram Daneshmandi, Aerospace 
Engineer, International Section, Transport Standards Branch, FAA, 1601 
Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1112; fax 
425-227-1149.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply to certain Saab AB, Saab 
Aeronautics Model SAAB 340B airplanes. The NPRM published in the 
Federal Register on August 15, 2017 (82 FR 38621) (``the NPRM'').
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2017-0067, dated April 24, 2017 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for certain Saab AB, Saab 
Aeronautics Model SAAB 340B airplanes. The MCAI states:

    A few natural stall events, specifically when operating in icing 
conditions, have been experienced on SAAB 340 series aeroplanes, 
without receiving a prior stall warning.
    This condition, if not corrected, could result in loss of 
control of the aeroplane.
    To address this potential unsafe condition, SAAB developed a 
modified stall warning system, incorporating improved stall warning 
logic, and issued various Service Bulletins (SB) providing 
instructions to replace the Stall Warning Computer (SWC) with a new 
SWC, and instructions to activate the new SWC. The new system 
includes stall warning curves optimized for operation in icing 
conditions, which are activated by selection of Engine Anti-Ice.
    Consequently, EASA issued AD 2014-0218 [which corresponds to FAA 
AD 2016-22-15, Amendment 39-18704 (81 FR 76843, November 4, 2016)] 
to require installation and activation of the improved SWC. That 
[EASA] AD excluded certain SAAB 340B aeroplanes by s/n [serial 
number].
    Since EASA AD 2014-0218 was issued, SAAB developed a technical 
solution applicable for some of those previously excluded 
aeroplanes, and issued SB 340-27-117 and SB 340-27-118, providing 
instructions to modify and activate the new SWC.
    For the reasons described above, this [EASA] AD requires 
installation and activation of the improved SWC.

    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-2017-
0777.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD as proposed except for 
minor editorial changes. We have determined that these minor changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Saab AB, Saab Aeronautics has issued Service Bulletin 340-27-117, 
dated January 23, 2017. This service information describes procedures 
for modifying the stall warning system.
    Saab AB, Saab Aeronautics has also issued Service Bulletin 340-27-
118, dated January 23, 2017. This service information describes 
procedures for installing new stall warning computers and activating 
the modified stall warning system.
    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

    We estimate that this AD affects 4 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Modification, installation, and         78 work-hours x $85 per          $33,000         $39,630        $158,520
 activation.                             hour = $6,630.
----------------------------------------------------------------------------------------------------------------

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.
    We are 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 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

[[Page 51342]]

airplanes to the Director of the System Oversight Division.

Regulatory Findings

    We determined that 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. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979);
    3. Will not affect intrastate aviation in Alaska; and
    4. 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

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 (AD):

2017-22-09 Saab AB, Saab Aeronautics (Formerly Known as Saab AB, 
Saab Aerosystems): Amendment 39-19089; Docket No. FAA-2017-0777; 
Product Identifier 2017-NM-050-AD.

(a) Effective Date

    This AD is effective December 11, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Saab AB, Saab Aeronautics (formerly known as 
Saab AB, Saab Aerosystems) Model SAAB 340B airplanes, certificated 
in any category, serial numbers 362, 363, 385, and 405.

(d) Subject

    Air Transport Association (ATA) of America Code 27, Flight 
Controls.

(e) Reason

    This AD was prompted by reports of natural stall events in icing 
conditions, without prior stall warnings. We are issuing this AD to 
prevent a natural stall event in icing conditions without any stall 
warning, which could result in loss of control of the airplane.

(f) Compliance

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

(g) Modification

    Within 12 months after the effective date of this AD, do the 
actions specified in paragraphs (g)(1) and (g)(2) of this AD.
    (1) Install a provision for a modified stall warning system, in 
accordance with the Accomplishment Instructions of Saab Service 
Bulletin 340-27-117, dated January 23, 2017.
    (2) Install new stall warning computers and activate the 
modified stall warning system, in accordance with the Accomplishment 
Instructions of Saab Service Bulletin 340-27-118, dated January 23, 
2017.

(h) Parts Installation Prohibition

    After modification of an airplane as required by paragraph (g) 
of this AD, no person may install a stall warning computer having 
part number (P/N) 20AK5 or P/N 0020AK5 on that airplane.

(i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards 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 Section, send it to the attention of 
the person identified in paragraph (j)(2) of this AD. Information 
may be emailed to: <a href="/cdn-cgi/l/email-protection#1f26325e5152322e2e29325e52505c324d5a4e4a5a4c4b4c5f797e7e31787069"><span class="__cf_email__" data-cfemail="724b5f333c3f5f4343445f333f3d315f2037232737212621321413135c151d04">[email protected]</span></a>. 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, International 
Section, Transport Standards Branch, FAA; or the European Aviation 
Safety Agency (EASA); or Saab AB, Saab Aeronautics's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

(j) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2017-0067, dated April 24, 2017, 
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-2017-0777.
    (2) For more information about this AD, contact Shahram 
Daneshmandi, Aerospace Engineer, International Section, Transport 
Standards Branch, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; 
telephone 425-227-1112; fax 425-227-1149.

(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) Saab Service Bulletin 340-27-117, dated January 23, 2017.
    (ii) Saab Service Bulletin 340-27-118, dated January 23, 2017.
    (3) For service information identified in this AD, contact Saab 
AB, Saab Aeronautics, SE-581 88, Link[ouml]ping, Sweden; telephone 
+46 13 18 5591; fax +46 13 18 4874; email 
<a href="/cdn-cgi/l/email-protection#1c6f7d7d7e2f282c3268797f746f696c6c736e685c6f7d7d7e7b6e73696c327f7371"><span class="__cf_email__" data-cfemail="c6b5a7a7a4f5f2f6e8b2a3a5aeb5b3b6b6a9b4b286b5a7a7a4a1b4a9b3b6e8a5a9ab">[email protected]</span></a>; Internet http://www.saabgroup.com.
    (4) You may view this service information at the FAA, Transport 
Standards Branch, 1601 Lind Avenue SW., Renton, WA. For information 
on the availability of this material at the FAA, call 425-227-1221.
    (5) 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, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on October 19, 2017.
Jeffrey E. Duven,
Director, System Oversight Division, Aircraft Certification Service.
[FR Doc. 2017-23344 Filed 11-3-17; 8:45 am]
 BILLING CODE 4910-13-P


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