[Federal Register Volume 82, Number 7 (Wednesday, January 11, 2017)]
[Rules and Regulations]
[Pages 3143-3146]
[FR Doc No: 2016-31958]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9113; Directorate Identifier 2016-NM-042-AD;
Amendment 39-18772; AD 2017-01-05]
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.

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SUMMARY: We are adopting a new airworthiness directive (AD) for all
Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN 235-200, and
CN-235-300 airplanes. This AD was prompted by reports of cracks in
certain areas of the rear fuselage. This AD requires repetitive
borescope and detailed visual inspections of the rear fuselage lateral
beam and its external area, and repair if necessary. We are issuing
this AD to address the unsafe condition on these products.

DATES: This AD is effective February 15, 2017.
    The Director of the Federal Register approved the incorporation by
reference of a certain publications listed in this AD as of February
15, 2017.

ADDRESSES: For service information identified in this final rule,
contact Airbus Defence 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_ADDRESS>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<PHONE_NUMBER>. It is also
available on the Internet at http://www.regulations.gov by searching
for and locating Docket No. FAA-2016-9113.

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-2016-
9113; 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 Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356;
telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

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 CN-235, CN-235-100, CN-235-200, and CN-235-300
airplanes. The NPRM published in the Federal Register on September 29,
2016 (81 FR 66872). The NPRM was prompted by reports of cracks in
certain areas of the rear fuselage. The NPRM proposed to require
repetitive borescope and detailed visual inspections of the rear
fuselage lateral beam and its external area, and repair if necessary.
We are issuing this AD to address the unsafe condition on these
products.
    The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued
Airworthiness Directive 2016-0064, dated April 4, 2016 (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 CN-235, CN-235-100, CN-235-200, and CN-235-300
airplanes. The MCAI states:

    During a scheduled visual inspection accomplished in accordance
with the CN-235 Maintenance Review Board (MRB) Document task 53.160,
cracking was found, affecting the rear fuselage lateral beam, both
left hand (LH) and right hand (RH) sides. The investigation to
determine the cause of these cracks is on-going.
    This condition, if not detected and corrected, could lead to
failure of the affected components, resulting in reduced structural
integrity of the fuselage.
    To address this potential unsafe condition, Airbus Defence and
Space (D&S) issued Alert Operator Transmission (AOT) AOT-CN235-53-
0002 Revision 1 (hereafter referred to as `the AOT' in this AD) to
provide inspection instructions.
    For the reasons described above, this [EASA] AD requires
repetitive inspections [special detailed inspection with a borescope
and detailed visual] of the rear fuselage lateral beam and its
external area and, depending on findings, [cracks or discrepancies],
accomplishment of applicable corrective action(s) [repair].

    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-2016-
9113.

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

    We reviewed Airbus Defense and Space Alert Operators Transmission
(AOT), AOT-CN235-53-0002, Revision 1, dated September 17, 2015. This
service information describes repetitive borescope and detailed visual
inspection requirements for the rear fuselage lateral beam and its
external area. 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 13 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
----------------------------------------------------------------------------------------------------------------
Inspection.........................  2 work-hours x $85 per hour              $0            $170          $2,210
                                      = $170.
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    We have received no definitive data that will enable us to provide
cost estimates for the on-condition actions specified in this AD.

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 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):

2017-01-05 Airbus Defense and Space S.A. (Formerly Known as
Construcciones Aeronauticas, S.A.): Amendment 39-18772; Docket No.
FAA-2016-9113; Directorate Identifier 2016-NM-042-AD.

(a) Effective Date

    This AD is effective February 15, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus Defense and Space S.A. (formerly known
as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN-
235-200, and CN-235-300 airplanes, certificated in any category, all
manufacturer serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Reason

    This AD was prompted by reports of cracks in certain areas of
the rear fuselage. We are issuing this AD to detect and correct
cracks in the rear fuselage lateral beam and its external area; such
cracking could lead to failure of the affected components, and
result in reduced structural integrity of the fuselage.

(f) Compliance

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

(g) Repetitive Inspections on the Fuselage Lateral Beam

    Within the compliance time specified in table 1 to paragraph (g)
of this AD, and thereafter at intervals not to exceed the values
specified in table 2 to paragraph (g) of this AD, as applicable to
airplane model, accomplish the inspections as specified in
paragraphs (g)(1) and (g)(2) of this AD, in accordance with the
instructions of Airbus Defense and Space Alert Operators
Transmission (AOT) AOT-CN235-53-0002, Revision 1, dated September
17, 2015.
    (1) A special detailed inspection for cracks and other
discrepancies with a borescope of the rear fuselage lateral beam
between frame (FR) 31 and FR 45, left-hand (LH) and right-hand (RH)
side.
    (2) A detailed visual inspection for cracks and other
discrepancies of the external area of the rear fuselage lateral
beam, LH and RH side.

 Table 1 to Paragraph (g) of This AD--Initial Inspection Compliance Time
------------------------------------------------------------------------

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                     A or B, whichever occurs later
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A............................  Before exceeding 15,000 flight cycles or
                                15,000 flight hours, whichever occurs
                                first since airplane first flight.
B............................  Within 50 flight cycles or 50 flight
                                hours, whichever occurs first after the
                                effective date of this AD.
------------------------------------------------------------------------

  Table 2 to Paragraph (g) of This AD--Repetitive Inspection Intervals
------------------------------------------------------------------------
                                          Repetitive interval (whichever
            Airplane models               occurs first, flight cycles or
                                                  flight hours)
------------------------------------------------------------------------
Model CN-235 and CN-235-100 airplanes..  3,600 flight cycles or 3,100
                                          flight hours.
Model CN-235-200 airplanes.............  3,600 flight cycles or 2,800
                                          flight hours.
Model CN-235-300 airplanes.............  15,000 flight cycles or 15,000
                                          flight hours.
------------------------------------------------------------------------

(h) Repair

    If any crack or discrepancy is found during any inspection
required by paragraph (g) of this AD: Before further flight, contact
and obtain repair instructions from Airbus Defense and Space S.A. in
accordance with paragraph (k)(2) of this AD, and within the
compliance time indicated in those instructions, accomplish the
repair accordingly, including any post-repair maintenance task(s),
as applicable.

(i) Continued Inspection of Repaired Areas

    Accomplishment of a repair on an airplane, as required by
paragraph (h) of this AD, does not constitute terminating action for
the repetitive inspections as required by paragraph (g) of this AD
for that airplane, unless specified in the applicable repair
instructions obtained in paragraph (h).

(j) Credit for Previous Actions

    This paragraph provides credit for actions required by
paragraphs (g) and (h) of this AD, if those actions were performed
before the effective date of this AD, using Airbus Defense and Space
AOT AOT-CN235-53-0002, dated August 28, 2015.

(k) 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<PHONE_NUMBER>; fax<PHONE_NUMBER>. 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
Branch, ANM-116, Transport Airplane Directorate, FAA; or EASA; or
Airbus Defense and Space S.A.'s EASA Design Organization Approval
(DOA). If approved by the DOA, the approval must include the DOA-
authorized signature.

(l) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2016-0064, dated April 4, 2016,
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-2016-9113.
    (2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (m)(3) and (m)(4) of this AD.

(m) 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) Airbus Defense and Space Alert Operators Transmission (AOT),
AOT-CN235-53-0002, Revision 1, dated September 17, 2015.
    (ii) Reserved.
    (3) 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_ADDRESS>
Internet http://www.eads.net.
    (4) 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.
    (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<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on December 27, 2016.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-31958 Filed 1-10-17; 8:45 am]
 BILLING CODE 4910-13-P