82_FR_44016 82 FR 43835 - Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes

82 FR 43835 - Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 181 (September 20, 2017)

Page Range43835-43836
FR Document2017-19659

We are adopting a new airworthiness directive (AD) for all Airbus Defense and Space S.A. Model C-212-CB, C-212-CC, C-212-CD, C- 212-CE, and C-212-DF airplanes. This AD was prompted by reports of failures of the rudder pedal control system support. This AD requires modifying the rudder pedal adjustment system. We are issuing this AD to address the unsafe condition on these products.

Federal Register, Volume 82 Issue 181 (Wednesday, September 20, 2017) 
[Federal Register Volume 82, Number 181 (Wednesday, September 20, 2017)]
[Rules and Regulations]
[Pages 43835-43836]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-19659]



[[Page 43835]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0623; Product Identifier 2017-NM-024-AD; Amendment 
39-19038; AD 2017-19-08]
RIN 2120-AA64


Airworthiness Directives; Airbus Defense and Space S.A. (Formerly 
Known as Construcciones Aeronauticas, S.A.) Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for all 
Airbus Defense and Space S.A. Model C-212-CB, C-212-CC, C-212-CD, C-
212-CE, and C-212-DF airplanes. This AD was prompted by reports of 
failures of the rudder pedal control system support. This AD requires 
modifying the rudder pedal adjustment system. We are issuing this AD to 
address the unsafe condition on these products.

DATES: This AD is effective October 25, 2017.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 25, 
2017.

ADDRESSES: For service information identified in this final rule, 
contact Airbus Defense and Space Services/Engineering Support, Avenida 
de Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; 
fax +34 91 585 31 27; email [email protected]. You may 
view this referenced 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. It is 
also available on the Internet at http://www.regulations.gov by 
searching for and locating Docket No. FAA-2017-0623.

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-
0623; 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 all Airbus Defense and 
Space S.A. Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, and C-212-DF 
airplanes. The NPRM published in the Federal Register on June 27, 2017 
(82 FR 29019) (``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 2017-0036, dated February 21, 2017 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for all Airbus Defense 
and Space S.A. Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, and C-212-
DF airplanes. The MCAI states:

    Failures were reported of the pedal control system support of 
CASA C-212 aeroplanes. Subsequent investigation revealed that the 
welding area of the affected support structure had broken.
    This condition, if not corrected, could lead to failure of the 
rudder control system, possibly resulting in reduced control of the 
aeroplane.
    To address this potential unsafe condition, EADS-CASA issued 
Service Bulletin (SB) SB-212-27-0057 to provide modification 
instructions.
    For the reasons described above, this [EASA] AD requires 
modification of the rudder pedal adjustment system.

    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-
0623.

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:
     Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Airbus Defense and Space S.A. has issued EADS CASA Service Bulletin 
SB-212-27-0057, dated May 21, 2014. This service information describes 
procedures for modifying the rudder pedal adjustment 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 42 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........................  9 work-hours x $85 per           $5,683           $6,448         $270,816
                                       hour = $765.
----------------------------------------------------------------------------------------------------------------

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.

[[Page 43836]]

    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 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):

2017-19-08 Airbus Defense and Space S.A. (Formerly Known as 
Construcciones Aeronauticas, S.A.): Amendment 39-19038; Docket No. 
FAA-2017-0623; Product Identifier 2017-NM-024-AD.

(a) Effective Date

    This AD is effective October 25, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Airbus Defense and Space S.A. Model C-
212-CB, C-212-CC, C-212-CD, C-212-CE, and C-212-DF airplanes, 
certificated in any category.

(d) Subject

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

(e) Reason

    This AD was prompted by reports of failures of the rudder pedal 
control system support and a determination that the welding area of 
the affected support structure had broken. We are issuing this AD to 
prevent failure of the rudder control system, which could result in 
reduced controllability 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: Modify the 
rudder pedal adjustment system, in accordance with the 
Accomplishment Instructions of EADS CASA Service Bulletin SB-212-27-
0057, dated May 21, 2014.

(h) 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 (i)(2) of this AD. Information 
may be emailed to: [email protected]. 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 EADS CASA's EASA Design Organization 
Approval (DOA). If approved by the DOA, the approval must include 
the DOA-authorized signature.

(i) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2017-0036, dated February 21, 
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-2017-0623.
    (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.

(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 this AD specifies otherwise.
    (i) EADS CASA Service Bulletin SB-212-27-0057, dated May 21, 
2014.
    (ii) Reserved.
    (3) For service information identified in this AD, contact 
Airbus Defense and Space Services/Engineering Support, Avenida de 
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; 
fax +34 91 585 31 27; email [email protected].
    (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 September 7, 2017.
Jeffrey E. Duven,
Director, System Oversight Division, Aircraft Certification Service.
[FR Doc. 2017-19659 Filed 9-19-17; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 82, No. 181 / Wednesday, September 20, 2017 / Rules and Regulations 43835 DEPARTMENT OF TRANSPORTATION Examining the AD Docket This condition, if not corrected, could lead to failure of the rudder control system, You may examine the AD docket on possibly resulting in reduced control of the Federal Aviation Administration the Internet at http:// aeroplane. www.regulations.gov by searching for To address this potential unsafe condition, 14 CFR Part 39 and locating Docket No. FAA–2017– EADS–CASA issued Service Bulletin (SB) [Docket No. FAA–2017–0623; Product 0623; or in person at the Docket SB–212–27–0057 to provide modification Management Facility between 9 a.m. instructions. Identifier 2017–NM–024–AD; Amendment and 5 p.m., Monday through Friday, For the reasons described above, this 39–19038; AD 2017–19–08] except Federal holidays. The AD docket [EASA] AD requires modification of the contains this AD, the regulatory rudder pedal adjustment system. RIN 2120–AA64 evaluation, any comments received, and You may examine the MCAI in the Airworthiness Directives; Airbus other information. The street address for AD docket on the Internet at http:// Defense and Space S.A. (Formerly the Docket Office (telephone 800–647– www.regulations.gov by searching for Known as Construcciones 5527) is Docket Management Facility, and locating Docket No. FAA–2017– Aeronauticas, S.A.) Airplanes U.S. Department of Transportation, 0623. AGENCY: Federal Aviation Docket Operations, M–30, West Comments Administration (FAA), Department of Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., We gave the public the opportunity to Transportation (DOT). Washington, DC 20590. participate in developing this AD. We ACTION: Final rule. received no comments on the NPRM or FOR FURTHER INFORMATION CONTACT: SUMMARY: We are adopting a new Shahram Daneshmandi, Aerospace on the determination of the cost to the airworthiness directive (AD) for all Engineer, International Section, public. Airbus Defense and Space S.A. Model Transport Standards Branch, FAA, 1601 Conclusion C–212–CB, C–212–CC, C–212–CD, C– Lind Avenue SW., Renton, WA 98057– 3356; telephone 425–227–1112; fax We reviewed the relevant data and 212–CE, and C–212–DF airplanes. This 425–227–1149. determined that air safety and the AD was prompted by reports of failures SUPPLEMENTARY INFORMATION: public interest require adopting this AD of the rudder pedal control system as proposed except for minor editorial support. This AD requires modifying the Discussion changes. We have determined that these rudder pedal adjustment system. We are We issued a notice of proposed minor changes: issuing this AD to address the unsafe rulemaking (NPRM) to amend 14 CFR • Are consistent with the intent that condition on these products. part 39 by adding an AD that would was proposed in the NPRM for DATES: This AD is effective October 25, correcting the unsafe condition; and apply to all Airbus Defense and Space 2017. • Do not add any additional burden S.A. Model C–212–CB, C–212–CC, C– The Director of the Federal Register upon the public than was already 212–CD, C–212–CE, and C–212–DF approved the incorporation by reference proposed in the NPRM. airplanes. The NPRM published in the of a certain publication listed in this AD Federal Register on June 27, 2017 (82 Related Service Information Under 1 as of October 25, 2017. FR 29019) (‘‘the NPRM’’). CFR Part 51 ADDRESSES: For service information The European Aviation Safety Agency identified in this final rule, contact (EASA), which is the Technical Agent Airbus Defense and Space S.A. has Airbus Defense and Space Services/ for the Member States of the European issued EADS CASA Service Bulletin Engineering Support, Avenida de Union, has issued EASA Airworthiness SB–212–27–0057, dated May 21, 2014. Aragón 404, 28022 Madrid, Spain; Directive 2017–0036, dated February 21, This service information describes telephone +34 91 585 55 84; fax +34 91 2017 (referred to after this as the procedures for modifying the rudder 585 31 27; email Mandatory Continuing Airworthiness pedal adjustment system. This service MTA.TechnicalService@airbus.com. Information, or ‘‘the MCAI’’), to correct information is reasonably available You may view this referenced service an unsafe condition for all Airbus because the interested parties have information at the FAA, Transport Defense and Space S.A. Model C–212– access to it through their normal course Standards Branch, 1601 Lind Avenue CB, C–212–CC, C–212–CD, C–212–CE, of business or by the means identified SW., Renton, WA. For information on and C–212–DF airplanes. The MCAI in the ADDRESSES section. the availability of this material at the states: FAA, call 425–227–1221. It is also Costs of Compliance Failures were reported of the pedal control available on the Internet at http:// system support of CASA C–212 aeroplanes. We estimate that this AD affects 42 www.regulations.gov by searching for Subsequent investigation revealed that the airplanes of U.S. registry. and locating Docket No. FAA–2017– welding area of the affected support structure We estimate the following costs to 0623. had broken. comply with this AD: ESTIMATED COSTS Cost per Cost on U.S. Action Labor cost Parts cost product operators sradovich on DSKBBY8HB2PROD with RULES Modification ..................................................... 9 work-hours × $85 per hour = $765 ............. $5,683 $6,448 $270,816 Authority for This Rulemaking rules on aviation safety. Subtitle I, Aviation Programs,’’ describes in more section 106, describes the authority of detail the scope of the Agency’s Title 49 of the United States Code the FAA Administrator. ‘‘Subtitle VII: authority. specifies the FAA’s authority to issue VerDate Sep<11>2014 17:10 Sep 19, 2017 Jkt 241001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\20SER1.SGM 20SER1

43836 Federal Register / Vol. 82, No. 181 / Wednesday, September 20, 2017 / Rules and Regulations We are issuing this rulemaking under Authority: 49 U.S.C. 106(g), 40113, 44701. be accomplished using a method approved the authority described in ‘‘Subtitle VII, by the Manager, International Section, § 39.13 [Amended] Transport Standards Branch, FAA; or the Part A, Subpart III, Section 44701: General requirements.’’ Under that ■ 2. The FAA amends § 39.13 by adding European Aviation Safety Agency (EASA); or section, Congress charges the FAA with the following new airworthiness EADS CASA’s EASA Design Organization promoting safe flight of civil aircraft in directive (AD): Approval (DOA). If approved by the DOA, air commerce by prescribing regulations 2017–19–08 Airbus Defense and Space S.A. the approval must include the DOA- for practices, methods, and procedures (Formerly Known as Construcciones authorized signature. the Administrator finds necessary for Aeronauticas, S.A.): Amendment 39– (i) Related Information safety in air commerce. This regulation 19038; Docket No. FAA–2017–0623; is within the scope of that authority Product Identifier 2017–NM–024–AD. (1) Refer to Mandatory Continuing because it addresses an unsafe condition Airworthiness Information (MCAI) EASA (a) Effective Date Airworthiness Directive 2017–0036, dated that is likely to exist or develop on This AD is effective October 25, 2017. February 21, 2017, for related information. products identified in this rulemaking (b) Affected ADs This MCAI may be found in the AD docket action. This AD is issued in accordance with on the Internet at http://www.regulations.gov None. authority delegated by the Executive by searching for and locating Docket No. (c) Applicability FAA–2017–0623. Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. This AD applies to all Airbus Defense and (2) For more information about this AD, Space S.A. Model C–212–CB, C–212–CC, C– contact Shahram Daneshmandi, Aerospace In accordance with that order, issuance 212–CD, C–212–CE, and C–212–DF airplanes, Engineer, International Section, Transport of ADs is normally a function of the certificated in any category. Standards Branch, FAA, 1601 Lind Avenue Compliance and Airworthiness (d) Subject SW., Renton, WA 98057–3356; telephone Division, but during this transition 425–227–1112; fax 425–227–1149. period, the Executive Director has Air Transport Association (ATA) of delegated the authority to issue ADs America Code 27, Flight controls. (j) Material Incorporated by Reference applicable to transport category (e) Reason (1) The Director of the Federal Register airplanes to the Director of the System This AD was prompted by reports of approved the incorporation by reference Oversight Division. failures of the rudder pedal control system (IBR) of the service information listed in this Regulatory Findings support and a determination that the welding paragraph under 5 U.S.C. 552(a) and 1 CFR area of the affected support structure had part 51. We determined that this AD will not broken. We are issuing this AD to prevent (2) You must use this service information have federalism implications under failure of the rudder control system, which as applicable to do the actions required by Executive Order 13132. This AD will could result in reduced controllability of the this AD, unless this AD specifies otherwise. not have a substantial direct effect on airplane. (i) EADS CASA Service Bulletin SB–212– the States, on the relationship between (f) Compliance 27–0057, dated May 21, 2014. the national government and the States, (ii) Reserved. Comply with this AD within the or on the distribution of power and compliance times specified, unless already (3) For service information identified in responsibilities among the various done. this AD, contact Airbus Defense and Space levels of government. Services/Engineering Support, Avenida de For the reasons discussed above, I (g) Modification Aragón 404, 28022 Madrid, Spain; telephone certify that this AD: Within 12 months after the effective date +34 91 585 55 84; fax +34 91 585 31 27; email 1. Is not a ‘‘significant regulatory of this AD: Modify the rudder pedal MTA.TechnicalService@airbus.com. action’’ under Executive Order 12866; adjustment system, in accordance with the (4) You may view this service information 2. Is not a ‘‘significant rule’’ under the Accomplishment Instructions of EADS CASA Service Bulletin SB–212–27–0057, dated May at the FAA, Transport Standards Branch, DOT Regulatory Policies and Procedures 1601 Lind Avenue SW., Renton, WA. For (44 FR 11034, February 26, 1979); 21, 2014. information on the availability of this 3. Will not affect intrastate aviation in (h) Other FAA AD Provisions material at the FAA, call 425–227–1221. Alaska; and The following provisions also apply to this (5) You may view this service information 4. Will not have a significant AD: that is incorporated by reference at the economic impact, positive or negative, (1) Alternative Methods of Compliance National Archives and Records on a substantial number of small entities (AMOCs): The Manager, International Administration (NARA). For information on under the criteria of the Regulatory Section, Transport Standards Branch, FAA, the availability of this material at NARA, call Flexibility Act. has the authority to approve AMOCs for this 202–741–6030, or go to: http:// AD, if requested using the procedures found List of Subjects in 14 CFR Part 39 in 14 CFR 39.19. In accordance with 14 CFR www.archives.gov/federal-register/cfr/ibr- 39.19, send your request to your principal locations.html. Air transportation, Aircraft, Aviation safety, Incorporation by reference, inspector or local Flight Standards District Issued in Renton, Washington, on Office, as appropriate. If sending information September 7, 2017. Safety. directly to the International Section, send it to the attention of the person identified in Jeffrey E. Duven, Adoption of the Amendment paragraph (i)(2) of this AD. Information may Director, System Oversight Division, Aircraft Accordingly, under the authority be emailed to: 9-ANM-116-AMOC- Certification Service. delegated to me by the Administrator, REQUESTS@faa.gov. Before using any [FR Doc. 2017–19659 Filed 9–19–17; 8:45 am] the FAA amends 14 CFR part 39 as sradovich on DSKBBY8HB2PROD with RULES approved AMOC, notify your appropriate BILLING CODE 4910–13–P follows: principal inspector, or lacking a principal inspector, the manager of the local flight PART 39—AIRWORTHINESS standards district office/certificate holding DIRECTIVES district office. (2) Contacting the Manufacturer: For any ■ 1. The authority citation for part 39 requirement in this AD to obtain corrective continues to read as follows: actions from a manufacturer, the action must VerDate Sep<11>2014 17:10 Sep 19, 2017 Jkt 241001 PO 00000 Frm 00010 Fmt 4700 Sfmt 9990 E:\FR\FM\20SER1.SGM 20SER1


Document Created: 2018-10-24 14:21:02
Document Modified: 2018-10-24 14:21:02
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionRules and Regulations
ActionFinal rule.
DatesThis AD is effective October 25, 2017.
ContactShahram 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.
FR Citation82 FR 43835 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
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