80_FR_70116 80 FR 69898 - Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes

80 FR 69898 - 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 80, Issue 218 (November 12, 2015)

Page Range69898-69899
FR Document2015-28560

We propose to adopt a new airworthiness directive (AD) for certain Airbus Defense and Space S.A. (formerly known as Construcciones Aeronauticas, S.A.) Model CN-235-200 and CN-235-300 airplanes. This proposed AD was prompted by reports of false engine fire warning events, which consequently led to engine in-flight shut down. This proposed AD would require modification of the location and routing of the engine fire detection system. We are proposing this AD to prevent unnecessary engine in-flight shut down, which could result in reduced controllability of the airplane.

Federal Register, Volume 80 Issue 218 (Thursday, November 12, 2015) 
[Federal Register Volume 80, Number 218 (Thursday, November 12, 2015)]
[Proposed Rules]
[Pages 69898-69899]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-28560]



[[Page 69898]]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-4809; Directorate Identifier 2015-NM-012-AD]
RIN 2120-AA64


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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Airbus Defense and Space S.A. (formerly known as Construcciones 
Aeronauticas, S.A.) Model CN-235-200 and CN-235-300 airplanes. This 
proposed AD was prompted by reports of false engine fire warning 
events, which consequently led to engine in-flight shut down. This 
proposed AD would require modification of the location and routing of 
the engine fire detection system. We are proposing this AD to prevent 
unnecessary engine in-flight shut down, which could result in reduced 
controllability of the airplane.

DATES: We must receive comments on this proposed AD by December 28, 
2015.

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 http://www.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: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday 
through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact 
EADS-CASA, Military Transport Aircraft Division (MTAD), Integrated 
Customer Services (ICS), Technical Services, Avenida de Arag[oacute]n 
404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 55 
05; email [email protected]; Internet http://www.eads.net. You may view this referenced service information at the 
FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. 
For information on the availability of this material at the FAA, call 
425-227-1221.

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-2015-
4809; 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 proposed AD, the regulatory evaluation, any comments 
received, and other information. The street address for the Docket 
Operations office (telephone 800-647-5527) is in the ADDRESSES section. 
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace 
Engineer, International Branch, ANM-116, Transport Airplane 
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; 
telephone 425-227-1112; fax 425-227-1149.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2015-4809; 
Directorate Identifier 2015-NM-012-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD based on those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2015-0011, dated January 20, 2015 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for certain Defense and 
Space S.A. (formerly known as Construcciones Aeronauticas, S.A.) Model 
CN-235-200 and CN-235-300 airplanes. The MCAI states:

    Several cases of false engine fire warning events were reported, 
which consequently led to engine in-flight shut down (IFSD) executed 
by the flightcrew using the appropriate emergency procedures. 
Subsequent investigation determined that these false engine fire 
warnings were the result of insufficient insulation capability of 
the engine fire detection system. This allowed penetration of 
moisture into the fire detector connectors, reducing the insulation 
resistance between the inner electrode and connector housing below 
the required values.
    This condition, if not corrected, could lead to further cases of 
unnecessary engine IFSD, possibly resulting in reduced control of 
the aeroplane.
    To address this potential unsafe condition, EADS-CASA issued 
Service Bulletin (SB) SB235-26-0006 providing modification 
instructions.
    For the reasons described above, this [EASA] AD requires 
modification of the location and routing of the engine fire 
detection 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-2015-
4809.

Related Service Information Under 1 CFR Part 51

    EADS CASA has issued Service Bulletin SB-235-26-0006, dated July 8, 
2014. The service information describes procedures for modifying the 
engine fire detection 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 of this NPRM.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all pertinent information and determined an unsafe condition 
exists and is likely to exist or develop on other products of these 
same type designs.

Costs of Compliance

    We estimate that this proposed AD affects 24 airplanes of U.S. 
registry.
    We also estimate that it would take about 75 work-hours per product 
to comply with the basic requirements of this proposed AD. The average 
labor rate is $85 per work-hour. Required

[[Page 69899]]

parts would cost about $1,577 per product. Based on these figures, we 
estimate the cost of this proposed AD on U.S. operators to be $190,848, 
or $7,952 per product.

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.

Regulatory Findings

    We 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. 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.

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

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):

Airbus Defense and Space S.A. (formerly known as Construcciones 
Aeronauticas, S.A.): Docket No. FAA-2015-4809; Directorate 
Identifier 2015-NM-012-AD.

(a) Comments Due Date

    We must receive comments by December 28, 2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the Airbus Defense and Space S.A. (formerly 
known as Construcciones Aeronauticas, S.A.) Model CN-235-200 and CN-
235-300 airplanes, certificated in any category, manufacturer serial 
numbers C-018 through C-211 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Code 26, Fire 
Protection.

(e) Reason

    This AD was prompted by reports of false engine fire warning 
events, which consequently led to engine in-flight shut down. We are 
issuing this AD to prevent unnecessary in-flight-shutdown of an 
engine, 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 of Engine Fire Extinguishing/Detection System

    Within 18 months after the effective date of this AD: Modify the 
location and routing of the engine fire detection system, in 
accordance with the Accomplishment Instructions of EADS CASA Service 
Bulletin SB-235-26-0006, dated July 8, 2014.

(h) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Shahram 
Daneshmandi, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
WA 98057-3356; telephone 425-227-1112; fax 425-227-1149. 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. The 
AMOC approval letter must specifically reference this AD.
    (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 
Branch, ANM-116, Transport Airplane Directorate, 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 2015-0011, dated January 20, 
2015, 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-2015-4809.
    (2) For service information identified in this AD, contact EADS-
CASA, Military Transport Aircraft Division (MTAD), Integrated 
Customer Services (ICS), Technical Services, Avenida de 
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; 
fax +34 91 585 55 05; email [email protected]; 
Internet http://www.eads.net.You may view this service information 
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., 
Renton, WA. For information on the availability of this material at 
the FAA, call 425-227-1221.

    Issued in Renton, Washington, on October 30, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-28560 Filed 11-10-15; 8:45 am]
BILLING CODE 4910-13-P

69898 Federal Register / Vol. 80, No. 218 / Thursday, November 12, 2015 / Proposed Rules DEPARTMENT OF TRANSPORTATION view this referenced service information Model CN–235–200 and CN–235–300 at the FAA, Transport Airplane airplanes. The MCAI states: Federal Aviation Administration Directorate, 1601 Lind Avenue SW., Several cases of false engine fire warning Renton, WA. For information on the events were reported, which consequently 14 CFR Part 39 availability of this material at the FAA, led to engine in-flight shut down (IFSD) call 425–227–1221. executed by the flightcrew using the [Docket No. FAA–2015–4809; Directorate appropriate emergency procedures. Identifier 2015–NM–012–AD] Examining the AD Docket Subsequent investigation determined that RIN 2120–AA64 You may examine the AD docket on these false engine fire warnings were the result of insufficient insulation capability of the Internet at http:// the engine fire detection system. This Airworthiness Directives; Airbus www.regulations.gov by searching for Defense and Space S.A. (Formerly allowed penetration of moisture into the fire and locating Docket No. FAA–2015– detector connectors, reducing the insulation Known as Construcciones 4809; or in person at the Docket resistance between the inner electrode and Aeronauticas, S.A.) Airplanes Management Facility between 9 a.m. connector housing below the required values. AGENCY: Federal Aviation and 5 p.m., Monday through Friday, This condition, if not corrected, could lead except Federal holidays. The AD docket to further cases of unnecessary engine IFSD, Administration (FAA), DOT. contains this proposed AD, the possibly resulting in reduced control of the ACTION: Notice of proposed rulemaking aeroplane. (NPRM). regulatory evaluation, any comments To address this potential unsafe condition, received, and other information. The EADS–CASA issued Service Bulletin (SB) SUMMARY: We propose to adopt a new street address for the Docket Operations SB235–26–0006 providing modification airworthiness directive (AD) for certain office (telephone 800–647–5527) is in instructions. Airbus Defense and Space S.A. the ADDRESSES section. Comments will For the reasons described above, this (formerly known as Construcciones be available in the AD docket shortly [EASA] AD requires modification of the Aeronauticas, S.A.) Model CN–235–200 after receipt. location and routing of the engine fire and CN–235–300 airplanes. This detection system. FOR FURTHER INFORMATION CONTACT: proposed AD was prompted by reports Shahram Daneshmandi, Aerospace You may examine the MCAI in the of false engine fire warning events, Engineer, International Branch, ANM– AD docket on the Internet at http:// which consequently led to engine in- 116, Transport Airplane Directorate, www.regulations.gov by searching for flight shut down. This proposed AD FAA, 1601 Lind Avenue SW., Renton, and locating Docket No. FAA–2015– would require modification of the WA 98057–3356; telephone 425–227– 4809. location and routing of the engine fire 1112; fax 425–227–1149. Related Service Information Under 1 detection system. We are proposing this SUPPLEMENTARY INFORMATION: CFR Part 51 AD to prevent unnecessary engine in- flight shut down, which could result in Comments Invited EADS CASA has issued Service reduced controllability of the airplane. Bulletin SB–235–26–0006, dated July 8, We invite you to send any written 2014. The service information describes DATES: We must receive comments on relevant data, views, or arguments about this proposed AD by December 28, procedures for modifying the engine fire this proposed AD. Send your comments detection system. This service 2015. to an address listed under the information is reasonably available ADDRESSES: You may send comments, ADDRESSES section. Include ‘‘Docket No. because the interested parties have using the procedures found in 14 CFR FAA–2015–4809; Directorate Identifier access to it through their normal course 11.43 and 11.45, by any of the following 2015–NM–012–AD’’ at the beginning of of business or by the means identified methods: your comments. We specifically invite in the ADDRESSES section of this NPRM. • Federal eRulemaking Portal: Go to comments on the overall regulatory, http://www.regulations.gov. Follow the economic, environmental, and energy FAA’s Determination and Requirements instructions for submitting comments. aspects of this proposed AD. We will of This Proposed AD • Fax: 202–493–2251. consider all comments received by the This product has been approved by • Mail: U.S. Department of closing date and may amend this the aviation authority of another Transportation, Docket Operations, M– proposed AD based on those comments. country, and is approved for operation 30, West Building Ground Floor, Room We will post all comments we in the United States. Pursuant to our W12–140, 1200 New Jersey Avenue SE., receive, without change, to http:// bilateral agreement with the State of Washington, DC 20590. www.regulations.gov, including any Design Authority, we have been notified • Hand Delivery: U.S. Department of personal information you provide. We of the unsafe condition described in the Transportation, Docket Operations, M– will also post a report summarizing each MCAI and service information 30, West Building Ground Floor, Room substantive verbal contact we receive referenced above. We are proposing this W12–140, 1200 New Jersey Avenue SE., about this proposed AD. AD because we evaluated all pertinent Washington, DC, between 9 a.m. and 5 information and determined an unsafe Discussion p.m., Monday through Friday, except condition exists and is likely to exist or Federal holidays. The European Aviation Safety Agency develop on other products of these same For service information identified in (EASA), which is the Technical Agent type designs. this proposed AD, contact EADS–CASA, for the Member States of the European mstockstill on DSK4VPTVN1PROD with PROPOSALS Military Transport Aircraft Division Union, has issued EASA Airworthiness Costs of Compliance (MTAD), Integrated Customer Services Directive 2015–0011, dated January 20, We estimate that this proposed AD (ICS), Technical Services, Avenida de 2015 (referred to after this as the affects 24 airplanes of U.S. registry. Aragón 404, 28022 Madrid, Spain; Mandatory Continuing Airworthiness We also estimate that it would take telephone +34 91 585 55 84; fax +34 91 Information, or ‘‘the MCAI’’), to correct about 75 work-hours per product to 585 55 05; email an unsafe condition for certain Defense comply with the basic requirements of MTA.TechnicalService@casa.eads.net; and Space S.A. (formerly known as this proposed AD. The average labor Internet http://www.eads.net. You may Construcciones Aeronauticas, S.A.) rate is $85 per work-hour. Required VerDate Sep<11>2014 17:34 Nov 10, 2015 Jkt 238001 PO 00000 Frm 00011 Fmt 4702 Sfmt 4702 E:\FR\FM\12NOP1.SGM 12NOP1

Federal Register / Vol. 80, No. 218 / Thursday, November 12, 2015 / Proposed Rules 69899 parts would cost about $1,577 per PART 39—AIRWORTHINESS Airplane Directorate, FAA, 1601 Lind product. Based on these figures, we DIRECTIVES Avenue SW., Renton, WA 98057–3356; estimate the cost of this proposed AD on telephone 425–227–1112; fax 425–227–1149. ■ 1. The authority citation for part 39 Information may be emailed to: 9-ANM-116- U.S. operators to be $190,848, or $7,952 AMOC-REQUESTS@faa.gov. Before using per product. continues to read as follows: any approved AMOC, notify your appropriate Authority for This Rulemaking Authority: 49 U.S.C. 106(g), 40113, 44701. principal inspector, or lacking a principal inspector, the manager of the local flight Title 49 of the United States Code § 39.13 [Amended] standards district office/certificate holding specifies the FAA’s authority to issue ■ 2. The FAA amends § 39.13 by adding district office. The AMOC approval letter rules on aviation safety. Subtitle I, the following new airworthiness must specifically reference this AD. (2) Contacting the Manufacturer: For any section 106, describes the authority of directive (AD): requirement in this AD to obtain corrective the FAA Administrator. ‘‘Subtitle VII: Airbus Defense and Space S.A. (formerly actions from a manufacturer, the action must Aviation Programs,’’ describes in more known as Construcciones Aeronauticas, be accomplished using a method approved detail the scope of the Agency’s S.A.): Docket No. FAA–2015–4809; by the Manager, International Branch, ANM– authority. Directorate Identifier 2015–NM–012–AD. 116, Transport Airplane Directorate, FAA; or We are issuing this rulemaking under the European Aviation Safety Agency (a) Comments Due Date (EASA); or EADS CASA’s EASA Design the authority described in ‘‘Subtitle VII, We must receive comments by December Organization Approval (DOA). If approved by Part A, Subpart III, Section 44701: 28, 2015. the DOA, the approval must include the General requirements.’’ Under that DOA-authorized signature. section, Congress charges the FAA with (b) Affected ADs None. (i) Related Information promoting safe flight of civil aircraft in air commerce by prescribing regulations (1) Refer to Mandatory Continuing (c) Applicability Airworthiness Information (MCAI) EASA for practices, methods, and procedures This AD applies to the Airbus Defense and Airworthiness Directive 2015–0011, dated the Administrator finds necessary for Space S.A. (formerly known as January 20, 2015, for related information. safety in air commerce. This regulation Construcciones Aeronauticas, S.A.) Model This MCAI may be found in the AD docket is within the scope of that authority CN–235–200 and CN–235–300 airplanes, on the Internet at http://www.regulations.gov because it addresses an unsafe condition certificated in any category, manufacturer by searching for and locating Docket No. that is likely to exist or develop on serial numbers C–018 through C–211 FAA–2015–4809. products identified in this rulemaking inclusive. (2) For service information identified in action. this AD, contact EADS–CASA, Military (d) Subject Transport Aircraft Division (MTAD), Regulatory Findings Air Transport Association (ATA) of Integrated Customer Services (ICS), America Code 26, Fire Protection. Technical Services, Avenida de Aragón 404, We determined that this proposed AD 28022 Madrid, Spain; telephone +34 91 585 would not have federalism implications (e) Reason 55 84; fax +34 91 585 55 05; email under Executive Order 13132. This This AD was prompted by reports of false MTA.TechnicalService@casa.eads.net; proposed AD would not have a engine fire warning events, which Internet http://www.eads.net.You may view substantial direct effect on the States, on consequently led to engine in-flight shut this service information at the FAA, down. We are issuing this AD to prevent Transport Airplane Directorate, 1601 Lind the relationship between the national Avenue SW., Renton, WA. For information unnecessary in-flight-shutdown of an engine, Government and the States, or on the which could result in reduced controllability on the availability of this material at the distribution of power and of the airplane. FAA, call 425–227–1221. responsibilities among the various Issued in Renton, Washington, on October levels of government. (f) Compliance 30, 2015. For the reasons discussed above, I Comply with this AD within the Michael Kaszycki, certify this proposed regulation: compliance times specified, unless already done. Acting Manager, Transport Airplane 1. Is not a ‘‘significant regulatory Directorate, Aircraft Certification Service. action’’ under Executive Order 12866; (g) Modification of Engine Fire [FR Doc. 2015–28560 Filed 11–10–15; 8:45 am] Extinguishing/Detection System 2. Is not a ‘‘significant rule’’ under the BILLING CODE 4910–13–P DOT Regulatory Policies and Procedures Within 18 months after the effective date (44 FR 11034, February 26, 1979); of this AD: Modify the location and routing of the engine fire detection system, in DEPARTMENT OF TRANSPORTATION 3. Will not affect intrastate aviation in accordance with the Accomplishment Alaska; and Instructions of EADS CASA Service Bulletin Federal Aviation Administration 4. Will not have a significant SB–235–26–0006, dated July 8, 2014. economic impact, positive or negative, (h) Other FAA AD Provisions 14 CFR Part 39 on a substantial number of small entities The following provisions also apply to this [Docket No. FAA–2015–4810; Directorate under the criteria of the Regulatory AD: Flexibility Act. Identifier 2015–NM–090–AD] (1) Alternative Methods of Compliance (AMOCs): The Manager, International RIN 2120–AA64 List of Subjects in 14 CFR Part 39 Branch, ANM–116, Transport Airplane Air transportation, Aircraft, Aviation Directorate, FAA, has the authority to Airworthiness Directives; Airbus mstockstill on DSK4VPTVN1PROD with PROPOSALS safety, Incorporation by reference, approve AMOCs for this AD, if requested Airplanes Safety. using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your AGENCY: Federal Aviation The Proposed Amendment request to your principal inspector or local Administration (FAA), DOT. Flight Standards District Office, as ACTION: Notice of proposed rulemaking Accordingly, under the authority appropriate. If sending information directly (NPRM). delegated to me by the Administrator, to the International Branch, send it to ATTN: the FAA proposes to amend 14 CFR part Shahram Daneshmandi, Aerospace Engineer, SUMMARY: We propose to adopt a new 39 as follows: International Branch, ANM–116, Transport airworthiness directive (AD) for all VerDate Sep<11>2014 17:34 Nov 10, 2015 Jkt 238001 PO 00000 Frm 00012 Fmt 4702 Sfmt 4702 E:\FR\FM\12NOP1.SGM 12NOP1


Document Created: 2015-12-14 14:53:16
Document Modified: 2015-12-14 14:53:16
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionProposed Rules
ActionNotice of proposed rulemaking (NPRM).
DatesWe must receive comments on this proposed AD by December 28, 2015.
ContactShahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1112; fax 425-227-1149.
FR Citation80 FR 69898 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR