80_FR_80486 80 FR 80239 - Airworthiness Directives; Airbus Airplanes

80 FR 80239 - Airworthiness Directives; Airbus Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 80, Issue 247 (December 24, 2015)

Page Range80239-80242
FR Document2015-31714

We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-200, A330-200 Freighter, and A330-300 series airplanes; and all Model A340-200 and A340-300 series airplanes. This AD was prompted by reports that a bracket that attaches the cockpit instrument panel to the airplane structure does not sustain the fatigue loads of the design service goal. This AD requires repetitive inspections of that bracket for cracking and to determine if both lugs are fully broken, an inspection for cracking of an adjacent bracket if necessary, and corrective actions if necessary. This AD also provides an optional modification, which terminates the repetitive inspections. We are issuing this AD to detect and correct cracking on a bracket of the cockpit instrument panel, which, combined with failure of the horizontal beam, could lead to collapse of the cockpit panel, and reduced controllability of the airplane.

Federal Register, Volume 80 Issue 247 (Thursday, December 24, 2015)
[Federal Register Volume 80, Number 247 (Thursday, December 24, 2015)]
[Rules and Regulations]
[Pages 80239-80242]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-31714]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-0083; Directorate Identifier 2014-NM-131-AD; 
Amendment 39-18347; AD 2015-25-09]
RIN 2120-AA64


Airworthiness Directives; Airbus Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Airbus Model A330-200, A330-200 Freighter, and A330-300 series 
airplanes; and all Model A340-200 and A340-300 series airplanes. This 
AD was prompted by reports that a bracket that attaches the cockpit 
instrument panel to the airplane structure does not sustain the fatigue 
loads of the design service goal. This AD requires repetitive 
inspections of that bracket for cracking and to determine if both lugs 
are fully broken, an inspection for cracking of an adjacent bracket if 
necessary, and corrective actions if necessary. This AD also provides 
an optional modification, which terminates the repetitive inspections. 
We are issuing this AD to detect and correct cracking on a bracket of 
the cockpit instrument panel, which, combined with failure of the 
horizontal beam, could lead to collapse of the cockpit panel, and 
reduced controllability of the airplane.

DATES: This AD becomes effective January 28, 2016.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of January 28, 
2016.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2015-0083; or in person at the 
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.
    For service information identified in this final rule, contact 
Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 
31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 
93 45 80; email [email protected]; Internet http://www.airbus.com. 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. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-
0083.

FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138; 
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 Airbus Model A330-
200, A330-200 Freighter, and A330-300 series airplanes; and all Model 
A340-200 and A340-300 series airplanes. The NPRM published in the 
Federal Register on February 13, 2015 (80 FR 7989).
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2014-0127, dated May 15, 2014 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for certain Airbus Model 
A330-200, A330-200 Freighter,

[[Page 80240]]

and A330-300 series airplanes; and all Model A340-200, and A340-300 
series airplanes. The MCAI states:

    During flight tests, high stress levels have been measured on 
the bracket No 6 which attaches the cockpit instrument panel to the 
aeroplane structure, apparently introduced through the nose landing 
gear due to bumps on the runway. Airbus determined that the bracket 
does not sustain the fatigue loads during the Design Service Goal 
(DSG).
    This condition, if not detected and corrected, combined with 
failure of the horizontal beam, could lead to collapse of the 
cockpit panel, possibly resulting in reduced control of the 
aeroplane.
    To address this potential unsafe condition, Airbus developed a 
program to inspect the condition of the affected cockpit instrument 
panel bracket No 6, and designed a stronger (reinforced titanium 
undrilled) bracket. The new bracket can be installed in-service 
through Airbus Service Bulletin (SB) A330-25-3548 or SB A340-25-
4354, as applicable to aeroplane type.
    For the reasons described above, this [EASA] AD requires 
repetitive inspections of the cockpit instrument panel bracket No 6 
and, depending on findings, the accomplishment of applicable 
corrective actions. This [EASA] AD also provides the installation of 
the stronger bracket as optional terminating action for the 
repetitive actions required by this [EASA] AD.

The corrective actions include replacing bracket No. 6 and bracket No. 
7 with serviceable parts, and repair, as applicable.
    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-0083-0002.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We have considered the comment received. The following 
presents the comment received on the NPRM (80 FR 7989, February 13, 
2015) and the FAA's response.

Request To Identify Part Numbers in Paragraphs (g) and (h)

    Delta Airlines requested that paragraphs (g) and (h) of the 
proposed AD (80 FR 7989, February 13, 2015) be revised to specify the 
part numbers of the affected brackets. Delta suggested that paragraph 
(g) of the proposed AD be revised to include the part number after the 
reference to bracket No. 6 (part number (P/N) F2511012820000, pre-
modification Number 55128S18242; and P/N F2511373420000, post-
modification Number 55128S18242). Delta also requested that paragraph 
(h)(2) of the proposed AD be revised to include the part number after 
bracket No. 6 (P/N F2511012820000, pre-modification Number 55128S18242; 
and P/N F2511373420000, post-modification Number 55128S18242) and 
bracket No. 7 (P/N F2511012820000, pre-modification Number 55128S18242; 
and P/N F2511373420000, post-modification Number 55128S18242). Delta 
stated that Airbus Service Bulletin A330-25-3538, Revision 02, dated 
April 24, 2014, specifies to inspect only P/N F2511012820000, pre-
modification Number 55128S18242, and P/N F2511373420000, post-
modification Number 55128S18242, and identifies only those part numbers 
as ``affected'' brackets that are used on both bracket No. 6 and 
bracket No. 7.
    We agree to include the part numbers identified by the commenter in 
paragraphs (g) and (h)(2) of this AD. We have also included the part 
numbers in paragraphs (h)(1) and (h)(2)(i) of this AD. The ``Reason/
Description/Operational Consequences'' section of Airbus Service 
Bulletin A330-25-3538, Revision 02, dated April 24, 2014, specifies to 
inspect P/N F2511012820000, pre-modification Number 55128S18242, and P/
N F2511373420000, post-modification Number 55128S18242. Also, the 
Accomplishment Instructions of that service bulletin specify to replace 
P/N F2511012820000 or P/N F2511373420000, as applicable. We contacted 
Airbus for verification that only those part numbers are considered to 
be ``affected'' brackets and Airbus confirmed that only those part 
numbers are affected. The same affected and replacement parts are used 
on both Airbus Model A330-200, A330-200 Freighter, and A330-300 series 
airplanes; and A340-200 and A340-300 series airplanes.

Additional Change to This AD

    A typographical error in paragraph (c)(1) of the proposed AD (80 FR 
7989, February 13, 2015) has been corrected in this final rule. 
Paragraph (c)(1) of the proposed AD inadvertently included Model A330-
313 airplanes instead of Model A330-343 airplanes. The SUMMARY section 
and preamble of the NPRM stated that the applicability included Model 
A330-300 series airplanes, which include Model A330-343 airplanes.

Conclusion

    We reviewed the relevant data, considered the comment received, and 
determined that air safety and the public interest require adopting 
this AD with the changes described previously and minor editorial 
changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (80 FR 7989, February 13, 2015) for correcting the unsafe 
condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (80 FR 7989, February 13, 2015).
    We also determined that these changes will not increase the 
economic burden on any operator or increase the scope of this AD.

Related Service Information Under 1 CFR Part 51

    Airbus has issued the following service information.
     Airbus Service Bulletin A330-25-3538, Revision 02, dated 
April 24, 2014, which provides procedures for inspection of cockpit 
instrument panel bracket 6.
     Airbus Service Bulletin A330-25-3548, dated October 31, 
2013, which provides procedures for replacement of cockpit instrument 
panel bracket 6 with a reinforced titanium bracket.
     Airbus Service Bulletin A340-25-4351, Revision 01, dated 
January 31, 2014, which provides procedures for inspection of cockpit 
instrument panel bracket 6.
     Airbus Service Bulletin A340-25-4354, dated October 31, 
2013, which provides procedures for replacement of cockpit instrument 
panel bracket 6 with a reinforced titanium bracket.
    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 76 airplanes of U.S. registry.
    We also estimate that it will take about 8 work-hours per product 
to comply with the basic requirements of this AD. The average labor 
rate is $85 per work-hour. Based on these figures, we estimate the cost 
of this AD on U.S. operators to be $51,680, or $680 per product.
    We have received no definitive data that would enable us to provide 
cost estimates for the follow-on repairs specified in this AD.
    In addition, we estimate that any necessary replacements will take 
about 23 work-hours and require parts costing $0, for a cost of $1,955 
per product. We have no way of determining the number of aircraft that 
might need these actions.
    We estimate that the optional modification will take about 9 work 
hours and require parts costing $1,770, for a cost of $2,535.

[[Page 80241]]

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.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2015-0083; 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 Operations office (telephone 800-647-
5527) is in the ADDRESSES section.

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):

2015-25-09 Airbus: Amendment 39-18347. Docket No. FAA-2015-0083; 
Directorate Identifier 2014-NM-131-AD.

(a) Effective Date

    This AD becomes effective January 28, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the Airbus airplanes, certificated in any 
category, identified in paragraphs (c)(1) and (c)(2) of this AD.
    (1) Model A330-201, -202, -203, -223, -243, -223F, -243F, -301, 
-302, -303, -321, -322, -323, -341, -342, and -343 airplanes, all 
manufacturer serial numbers except those on which Airbus 
Modification 203287 has been embodied in production.
    (2) Model A340-211, -212, -213, -311, -312, and -313 airplanes, 
all manufacturer serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.

(e) Reason

    This AD was prompted by reports that a bracket that attaches the 
cockpit instrument panel to the airplane structure does not sustain 
the fatigue loads of the design service goal. We are issuing this AD 
to detect and correct cracking on a bracket of the cockpit 
instrument panel, which, combined with failure of the horizontal 
beam, could lead to collapse of the cockpit panel, and reduced 
controllability of the airplane.

(f) Compliance

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

(g) Inspection of Bracket No. 6 of the Cockpit Instrument Panel

    At the latest of the times specified in paragraphs (g)(1), 
(g)(2), and (g)(3) of this AD: Do a detailed inspection of bracket 
No. 6 (part number (P/N) F2511012820000, pre-modification Number 
55128S18242; or P/N F2511373420000, post-modification Number 
55128S18242) of the cockpit instrument panel for cracking and to 
determine if both bracket lugs are fully broken, in accordance with 
the Accomplishment Instructions of Airbus Service Bulletin A330-25-
3538, Revision 02, dated April 24, 2014; or Airbus Service Bulletin 
A340-25-4351, Revision 01, dated January 31, 2014; as applicable. 
Repeat the inspection thereafter at intervals not to exceed 2,600 
flight cycles.
    (1) Prior to accumulating 17,200 total flight cycles since the 
airplane's first flight.
    (2) Prior to bracket No. 6 of the cockpit instrument panel 
accumulating 17,200 total flight cycles since installation on an 
airplane.
    (3) Within 500 flight cycles after the effective date of this 
AD.

(h) Inspection and Corrective Actions

    (1) If, during any inspection required by paragraph (g) of this 
AD, any cracking of bracket No. 6 (P/N F2511012820000, pre-
modification Number 55128S18242; or P/N F2511373420000, Post-
modification Number 55128S18242) of the cockpit instrument panel is 
found, and both bracket lugs are not fully broken: Within 2,600 
flight cycles after that inspection, replace bracket No. 6 of the 
cockpit instrument panel with a serviceable part, in accordance with 
the Accomplishment Instructions of Airbus Service Bulletin A330-25-
3538, Revision 02, dated April 24, 2014; or Airbus Service Bulletin 
A340-25-4351, Revision 01, dated January 31, 2014; as applicable. 
Replacement of bracket No. 6 (P/N F2511012820000, pre-modification 
Number 55128S18242; or P/N F2511373420000, post-modification Number 
55128S18242) of the cockpit instrument panel does not constitute 
terminating action for the repetitive inspections required by 
paragraph (g) of this AD.
    (2) If, during any inspection required by paragraph (g) of this 
AD, any cracking of bracket No. 6 (P/N F2511012820000, pre-
modification Number 55128S18242; or P/N F2511373420000, Post-
modification Number 55128S18242) of the cockpit instrument panel is 
found and both bracket lugs are fully broken: Before further flight, 
do a detailed inspection of bracket No. 7 (P/N F2511012820000, pre-
modification Number 55128S18242; or P/N F2511373420000, Post-
modification Number 55128S18242) of the cockpit instrument panel for 
cracking, in accordance with the Accomplishment Instructions of 
Airbus Service Bulletin A330-25-3538, Revision 02, dated April 24, 
2014; or Airbus Service Bulletin A340-25-4351, Revision 01, dated 
January 31, 2014; as applicable.
    (i) If, during the inspection required by paragraph (h)(2) of 
this AD, no cracking is found in bracket No. 7 of the cockpit 
instrument panel: Before further flight, replace bracket No. 6 and 
bracket No. 7 of the cockpit instrument panel with serviceable 
parts, in accordance with the Accomplishment Instructions of Airbus 
Service Bulletin A330-25-3538, Revision 02, dated April 24, 2014; or 
Airbus Service Bulletin A340-25-4351, Revision 01, dated January 31, 
2014; as applicable. Replacement of bracket No. 6 (P/N 
F2511012820000, pre-

[[Page 80242]]

modification Number 55128S18242; or P/N F2511373420000, post-
modification Number 55128S18242) of the cockpit instrument panel 
does not constitute terminating action for the repetitive 
inspections required by paragraph (g) of this AD.
    (ii) If, during the inspection required by paragraph (h)(2) of 
this AD, any cracking is found in bracket No. 7 of the cockpit 
instrument panel: Although Airbus Service Bulletin A330-25-3538, 
Revision 02, dated April 24, 2014; and Airbus Service Bulletin A340-
25-4351, Revision 01, dated January 31, 2014; specify to contact 
Airbus for repair instructions, and specify that action as ``RC'' 
(Required for Compliance), repair the cracking before further flight 
using a repair method approved by the Manager, International Branch, 
ANM-116, Transport Airplane Directorate, FAA; or the European 
Aviation Safety Agency (EASA); or Airbus's EASA Design Organization 
Approval (DOA).

(i) Optional Terminating Modification for Paragraph (g) of This AD

    Modifying an airplane by replacing bracket No. 6 of the cockpit 
instrument panel with a new, reinforced bracket, in accordance with 
the Accomplishment Instructions of Airbus Service Bulletin A330-25-
3548, dated October 31, 2013; or Airbus Service Bulletin A340-25-
4354, dated October 31, 2013; as applicable; terminates the 
repetitive inspections required by paragraph (g) of this AD.

(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 the service information 
identified in paragraph (j)(1), (j)(2), or (j)(3) of this AD, which 
is not incorporated by reference in this AD.
    (1) Airbus Service Bulletin A330-25-3538, dated September 10, 
2013.
    (2) Airbus Service Bulletin A330-25-3538, Revision 01, dated 
April 24, 2014.
    (3) Airbus Service Bulletin A340-25-4351, dated September 10, 
2014.

(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: Vladimir 
Ulyanov, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
WA 98057-3356; telephone 425-227-1138; 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 EASA; 
or Airbus's EASA DOA. If approved by the DOA, the approval must 
include the DOA-authorized signature.
    (3) Required for Compliance (RC): Except as required by 
paragraph (h)(2)(ii) of this AD, if Airbus Service Bulletin A330-25-
3538, Revision 02, dated April 24, 2014; or Airbus Service Bulletin 
A340-25-4351, Revision 01, dated January 31, 2014; contain 
procedures or tests that are identified as RC, those procedures and 
tests must be done to comply with this AD; any procedures and tests 
that are not identified as RC are recommended. Those procedures and 
tests that are not identified as RC may be deviated from, using 
accepted methods in accordance with the operators maintenance or 
inspection program without obtaining approval of an AMOC, provided 
the procedures and tests identified as RC can be done and the 
airplane can be put back in an airworthy condition. Any 
substitutions or changes to procedures or tests identified as RC 
require approval of an AMOC.

(l) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2014-0127, dated May 15, 2014, 
for related information. This MCAI may be found in the AD docket on 
the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-
2015-0083-0002.
    (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 Service Bulletin A330-25-3538, Revision 02, dated 
April 24, 2014.
    (ii) Airbus Service Bulletin A330-25-3548, dated October 31, 
2013.
    (iii) Airbus Service Bulletin A340-25-4351, Revision 01, dated 
January 31, 2014.
    (iv) Airbus Service Bulletin A340-25-4354, dated October 31, 
2013.
    (3) For service information identified in this AD, contact 
Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice 
Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; 
fax +33 5 61 93 45 80; email [email protected]; 
Internet http://www.airbus.com.
    (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 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on December 9, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-31714 Filed 12-23-15; 8:45 am]
BILLING CODE 4910-13-P



                                                             Federal Register / Vol. 80, No. 247 / Thursday, December 24, 2015 / Rules and Regulations                                      80239

                                            conditions specified in both paragraphs (h)(1)              (iii) Bombardier Service Bulletin 601–0625,        combined with failure of the horizontal
                                            and (h)(2) of this AD are met.                           Revision 01, dated January 13, 2014.                  beam, could lead to collapse of the
                                               (1) The action was performed before the                  (3) For service information identified in          cockpit panel, and reduced
                                            effective date of this AD using Bombardier               this AD, contact Bombardier, Inc., 400 Côte          controllability of the airplane.
                                            Service Bulletin 605–24–007, Bombardier                  Vertu Road West, Dorval, Québec H4S 1Y9,
                                            Service Bulletin 604–24–026, or Bombardier               Canada; telephone 514–855–5000; fax 514               DATES: This AD becomes effective
                                            Service Bulletin 601–0625, all dated                     855–7401; email thd.crj@                              January 28, 2016.
                                            September 18, 2012. This service information             aero.bombardier.com; Internet http://                   The Director of the Federal Register
                                            is not incorporated by reference in this AD.             www.bombardier.com.                                   approved the incorporation by reference
                                               (2) The action specified in Service Request              (4) You may view this service information          of certain publications listed in this AD
                                            for Product Support Action (SRPSA) 27512,                at the FAA, Transport Airplane Directorate,           as of January 28, 2016.
                                            SRPSA 30806, SRPSA 32727, SRPSA 32864,                   1601 Lind Avenue SW., Renton, WA. For                 ADDRESSES: You may examine the AD
                                            or SRPSA 33161 has not been done.                        information on the availability of this
                                                                                                                                                           docket on the Internet at http://
                                            (i) Other FAA AD Provisions                              material at the FAA, call 425–227–1221.
                                                                                                        (5) You may view this service information          www.regulations.gov/
                                               The following provisions also apply to this           that is incorporated by reference at the              #!docketDetail;D=FAA-2015-0083; or in
                                            AD:                                                      National Archives and Records                         person at the Docket Management
                                               (1) Alternative Methods of Compliance                 Administration (NARA). For information on             Facility, U.S. Department of
                                            (AMOCs): The Manager, New York Aircraft                  the availability of this material at NARA, call       Transportation, Docket Operations,
                                            Certification Office (ACO), ANE–170, FAA,                202–741–6030, or go to: http://
                                            has the authority to approve AMOCs for this
                                                                                                                                                           M–30, West Building Ground Floor,
                                                                                                     www.archives.gov/federal-register/cfr/ibr-            Room W12–140, 1200 New Jersey
                                            AD, if requested using the procedures found              locations.html.
                                            in 14 CFR 39.19. In accordance with 14 CFR                                                                     Avenue SE., Washington, DC.
                                            39.19, send your request to your principal                 Issued in Renton, Washington on                       For service information identified in
                                            inspector or local Flight Standards District             December 8, 2015.                                     this final rule, contact Airbus SAS,
                                            Office, as appropriate. If sending information           Michael Kaszycki,                                     Airworthiness Office—EAL, 1 Rond
                                            directly to the New York ACO, send it to                 Acting Manager, Transport Airplane                    Point Maurice Bellonte, 31707 Blagnac
                                            ATTN: Program Manager, Continuing                        Directorate, Aircraft Certification Service.          Cedex, France; telephone +33 5 61 93 36
                                            Operational Safety, FAA, New York ACO,                                                                         96; fax +33 5 61 93 45 80; email
                                            1600 Stewart Avenue, Suite 410, Westbury,                [FR Doc. 2015–31604 Filed 12–23–15; 8:45 am]
                                            NY 11590; telephone 516–228–7300; fax                    BILLING CODE 4910–13–P                                airworthiness.A330–A340@airbus.com;
                                            516–794–553. Before using any approved                                                                         Internet http://www.airbus.com. You
                                            AMOC, notify your appropriate principal                                                                        may view this referenced service
                                            inspector, or lacking a principal inspector,             DEPARTMENT OF TRANSPORTATION                          information at the FAA, Transport
                                            the manager of the local flight standards                                                                      Airplane Directorate, 1601 Lind Avenue
                                            district office/certificate holding district             Federal Aviation Administration                       SW., Renton, WA. For information on
                                            office. The AMOC approval letter must                                                                          the availability of this material at the
                                            specifically reference this AD.                          14 CFR Part 39                                        FAA, call 425–227–1221. It is also
                                               (2) Contacting the Manufacturer: For any
                                            requirement in this AD to obtain corrective
                                                                                                                                                           available on the Internet at http://
                                                                                                     [Docket No. FAA–2015–0083; Directorate
                                            actions from a manufacturer, the action must             Identifier 2014–NM–131–AD; Amendment                  www.regulations.gov by searching for
                                            be accomplished using a method approved                  39–18347; AD 2015–25–09]                              and locating Docket No. FAA–2015–
                                            by the Manager, New York ACO, ANE–170,                                                                         0083.
                                            Engine and Propeller Directorate, FAA; or                RIN 2120–AA64
                                                                                                                                                           FOR FURTHER INFORMATION CONTACT:
                                            Transport Canada Civil Aviation (TCCA); or
                                            Bombardier, Inc.’s TCCA Design Approval                  Airworthiness Directives; Airbus                      Vladimir Ulyanov, Aerospace Engineer,
                                            Organization (DAO). If approved by the DAO,              Airplanes                                             International Branch, ANM–116,
                                            the approval must include the DAO-                                                                             Transport Airplane Directorate, FAA,
                                            authorized signature.                                    AGENCY:  Federal Aviation                             1601 Lind Avenue SW., Renton, WA
                                                                                                     Administration (FAA), Department of                   98057–3356; telephone 425–227–1138;
                                            (j) Related Information
                                                                                                     Transportation (DOT).                                 fax 425–227–1149.
                                               (1) Refer to Mandatory Continuing
                                                                                                     ACTION: Final rule.                                   SUPPLEMENTARY INFORMATION:
                                            Airworthiness Information (MCAI) Canadian
                                            Airworthiness Directive CF–2014–05, dated                SUMMARY:   We are adopting a new                      Discussion
                                            January 20, 2014, for related information.
                                            This MCAI may be found in the AD docket                  airworthiness directive (AD) for certain                We issued a notice of proposed
                                            on the Internet at http://                               Airbus Model A330–200, A330–200                       rulemaking (NPRM) to amend 14 CFR
                                            www.regulations.gov/#!documentDetail;D=                  Freighter, and A330–300 series                        part 39 by adding an AD that would
                                            FAA-2014-0625-0003.                                      airplanes; and all Model A340–200 and                 apply to certain Airbus Model A330–
                                               (2) Service information identified in this            A340–300 series airplanes. This AD was                200, A330–200 Freighter, and A330–300
                                            AD that is not incorporated by reference is              prompted by reports that a bracket that               series airplanes; and all Model A340–
                                            available at the addresses specified in                  attaches the cockpit instrument panel to              200 and A340–300 series airplanes. The
                                            paragraphs (k)(3) and (k)(4) of this AD.                 the airplane structure does not sustain               NPRM published in the Federal
                                            (k) Material Incorporated by Reference                   the fatigue loads of the design service               Register on February 13, 2015 (80 FR
                                               (1) The Director of the Federal Register              goal. This AD requires repetitive                     7989).
                                            approved the incorporation by reference                  inspections of that bracket for cracking                The European Aviation Safety Agency
                                            (IBR) of the service information listed in this          and to determine if both lugs are fully               (EASA), which is the Technical Agent
                                            paragraph under 5 U.S.C. 552(a) and 1 CFR                broken, an inspection for cracking of an              for the Member States of the European
                                            part 51.                                                 adjacent bracket if necessary, and                    Union, has issued EASA Airworthiness
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                                               (2) You must use this service information             corrective actions if necessary. This AD              Directive 2014–0127, dated May 15,
                                            as applicable to do the actions required by
                                            this AD, unless this AD specifies otherwise.
                                                                                                     also provides an optional modification,               2014 (referred to after this as the
                                               (i) Bombardier Service Bulletin 605–24–               which terminates the repetitive                       Mandatory Continuing Airworthiness
                                            007, Revision 01, dated January 13, 2014.                inspections. We are issuing this AD to                Information, or ‘‘the MCAI’’), to correct
                                               (ii) Bombardier Service Bulletin 604–24–              detect and correct cracking on a bracket              an unsafe condition for certain Airbus
                                            026, Revision 01, dated January 13, 2014.                of the cockpit instrument panel, which,               Model A330–200, A330–200 Freighter,


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                                            80240            Federal Register / Vol. 80, No. 247 / Thursday, December 24, 2015 / Rules and Regulations

                                            and A330–300 series airplanes; and all                   Number 55128S18242; and P/N                             • Are consistent with the intent that
                                            Model A340–200, and A340–300 series                      F2511373420000, post-modification                     was proposed in the NPRM (80 FR 7989,
                                            airplanes. The MCAI states:                              Number 55128S18242) and bracket No.                   February 13, 2015) for correcting the
                                               During flight tests, high stress levels have          7 (P/N F2511012820000, pre-                           unsafe condition; and
                                            been measured on the bracket No 6 which                  modification Number 55128S18242; and                    • Do not add any additional burden
                                            attaches the cockpit instrument panel to the             P/N F2511373420000, post-modification                 upon the public than was already
                                            aeroplane structure, apparently introduced               Number 55128S18242). Delta stated that                proposed in the NPRM (80 FR 7989,
                                            through the nose landing gear due to bumps               Airbus Service Bulletin A330–25–3538,                 February 13, 2015).
                                            on the runway. Airbus determined that the                Revision 02, dated April 24, 2014,                      We also determined that these
                                            bracket does not sustain the fatigue loads               specifies to inspect only P/N                         changes will not increase the economic
                                            during the Design Service Goal (DSG).                    F2511012820000, pre-modification
                                               This condition, if not detected and
                                                                                                                                                           burden on any operator or increase the
                                            corrected, combined with failure of the
                                                                                                     Number 55128S18242, and P/N                           scope of this AD.
                                            horizontal beam, could lead to collapse of the           F2511373420000, post-modification
                                                                                                     Number 55128S18242, and identifies                    Related Service Information Under 1
                                            cockpit panel, possibly resulting in reduced                                                                   CFR Part 51
                                            control of the aeroplane.                                only those part numbers as ‘‘affected’’
                                               To address this potential unsafe condition,           brackets that are used on both bracket                   Airbus has issued the following
                                            Airbus developed a program to inspect the                No. 6 and bracket No. 7.                              service information.
                                            condition of the affected cockpit instrument                We agree to include the part numbers                  • Airbus Service Bulletin A330–25–
                                            panel bracket No 6, and designed a stronger                                                                    3538, Revision 02, dated April 24, 2014,
                                                                                                     identified by the commenter in
                                            (reinforced titanium undrilled) bracket. The
                                                                                                     paragraphs (g) and (h)(2) of this AD. We              which provides procedures for
                                            new bracket can be installed in-service
                                            through Airbus Service Bulletin (SB) A330–               have also included the part numbers in                inspection of cockpit instrument panel
                                            25–3548 or SB A340–25–4354, as applicable                paragraphs (h)(1) and (h)(2)(i) of this               bracket 6.
                                            to aeroplane type.                                       AD. The ‘‘Reason/Description/                            • Airbus Service Bulletin A330–25–
                                               For the reasons described above, this                 Operational Consequences’’ section of                 3548, dated October 31, 2013, which
                                            [EASA] AD requires repetitive inspections of             Airbus Service Bulletin A330–25–3538,                 provides procedures for replacement of
                                            the cockpit instrument panel bracket No 6                Revision 02, dated April 24, 2014,                    cockpit instrument panel bracket 6 with
                                            and, depending on findings, the                          specifies to inspect P/N                              a reinforced titanium bracket.
                                            accomplishment of applicable corrective                                                                           • Airbus Service Bulletin A340–25–
                                                                                                     F2511012820000, pre-modification
                                            actions. This [EASA] AD also provides the
                                            installation of the stronger bracket as                  Number 55128S18242, and P/N                           4351, Revision 01, dated January 31,
                                            optional terminating action for the repetitive           F2511373420000, post-modification                     2014, which provides procedures for
                                            actions required by this [EASA] AD.                      Number 55128S18242. Also, the                         inspection of cockpit instrument panel
                                            The corrective actions include replacing                 Accomplishment Instructions of that                   bracket 6.
                                            bracket No. 6 and bracket No. 7 with                     service bulletin specify to replace P/N                  • Airbus Service Bulletin A340–25–
                                            serviceable parts, and repair, as                        F2511012820000 or P/N                                 4354, dated October 31, 2013, which
                                            applicable.                                              F2511373420000, as applicable. We                     provides procedures for replacement of
                                              You may examine the MCAI in the                        contacted Airbus for verification that                cockpit instrument panel bracket 6 with
                                            AD docket on the Internet at http://                     only those part numbers are considered                a reinforced titanium bracket.
                                            www.regulations.gov/                                     to be ‘‘affected’’ brackets and Airbus                   This service information is reasonably
                                            #!documentDetail;D=FAA-2015-0083-                        confirmed that only those part numbers                available because the interested parties
                                            0002.                                                    are affected. The same affected and                   have access to it through their normal
                                                                                                     replacement parts are used on both                    course of business or by the means
                                            Comments                                                 Airbus Model A330–200, A330–200                       identified in the ADDRESSES section.
                                              We gave the public the opportunity to                  Freighter, and A330–300 series
                                                                                                                                                           Costs of Compliance
                                            participate in developing this AD. We                    airplanes; and A340–200 and A340–300
                                            have considered the comment received.                    series airplanes.                                       We estimate that this AD affects 76
                                            The following presents the comment                                                                             airplanes of U.S. registry.
                                                                                                     Additional Change to This AD
                                            received on the NPRM (80 FR 7989,                                                                                We also estimate that it will take
                                            February 13, 2015) and the FAA’s                            A typographical error in paragraph                 about 8 work-hours per product to
                                            response.                                                (c)(1) of the proposed AD (80 FR 7989,                comply with the basic requirements of
                                                                                                     February 13, 2015) has been corrected in              this AD. The average labor rate is $85
                                            Request To Identify Part Numbers in                      this final rule. Paragraph (c)(1) of the              per work-hour. Based on these figures,
                                            Paragraphs (g) and (h)                                   proposed AD inadvertently included                    we estimate the cost of this AD on U.S.
                                              Delta Airlines requested that                          Model A330–313 airplanes instead of                   operators to be $51,680, or $680 per
                                            paragraphs (g) and (h) of the proposed                   Model A330–343 airplanes. The                         product.
                                            AD (80 FR 7989, February 13, 2015) be                    SUMMARY section and preamble of the                     We have received no definitive data
                                            revised to specify the part numbers of                   NPRM stated that the applicability                    that would enable us to provide cost
                                            the affected brackets. Delta suggested                   included Model A330–300 series                        estimates for the follow-on repairs
                                            that paragraph (g) of the proposed AD be                 airplanes, which include Model A330–                  specified in this AD.
                                            revised to include the part number after                 343 airplanes.                                          In addition, we estimate that any
                                            the reference to bracket No. 6 (part                                                                           necessary replacements will take about
                                                                                                     Conclusion
                                            number (P/N) F2511012820000, pre-                                                                              23 work-hours and require parts costing
                                            modification Number 55128S18242; and                       We reviewed the relevant data,                      $0, for a cost of $1,955 per product. We
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                                            P/N F2511373420000, post-modification                    considered the comment received, and                  have no way of determining the number
                                            Number 55128S18242). Delta also                          determined that air safety and the                    of aircraft that might need these actions.
                                            requested that paragraph (h)(2) of the                   public interest require adopting this AD                We estimate that the optional
                                            proposed AD be revised to include the                    with the changes described previously                 modification will take about 9 work
                                            part number after bracket No. 6 (P/N                     and minor editorial changes. We have                  hours and require parts costing $1,770,
                                            F2511012820000, pre-modification                         determined that these minor changes:                  for a cost of $2,535.


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                                                             Federal Register / Vol. 80, No. 247 / Thursday, December 24, 2015 / Rules and Regulations                                            80241

                                            Authority for This Rulemaking                            List of Subjects in 14 CFR Part 39                    modification Number 55128S18242; or P/N
                                                                                                                                                           F2511373420000, post-modification Number
                                               Title 49 of the United States Code                      Air transportation, Aircraft, Aviation              55128S18242) of the cockpit instrument
                                            specifies the FAA’s authority to issue                   safety, Incorporation by reference,                   panel for cracking and to determine if both
                                            rules on aviation safety. Subtitle I,                    Safety.                                               bracket lugs are fully broken, in accordance
                                            section 106, describes the authority of                                                                        with the Accomplishment Instructions of
                                                                                                     Adoption of the Amendment                             Airbus Service Bulletin A330–25–3538,
                                            the FAA Administrator. ‘‘Subtitle VII:                     Accordingly, under the authority                    Revision 02, dated April 24, 2014; or Airbus
                                            Aviation Programs,’’ describes in more                   delegated to me by the Administrator,                 Service Bulletin A340–25–4351, Revision 01,
                                            detail the scope of the Agency’s                         the FAA amends 14 CFR part 39 as                      dated January 31, 2014; as applicable. Repeat
                                            authority.                                               follows:                                              the inspection thereafter at intervals not to
                                               We are issuing this rulemaking under                                                                        exceed 2,600 flight cycles.
                                                                                                     PART 39—AIRWORTHINESS                                    (1) Prior to accumulating 17,200 total flight
                                            the authority described in ‘‘Subtitle VII,
                                                                                                                                                           cycles since the airplane’s first flight.
                                            Part A, Subpart III, Section 44701:                      DIRECTIVES
                                                                                                                                                              (2) Prior to bracket No. 6 of the cockpit
                                            General requirements.’’ Under that                                                                             instrument panel accumulating 17,200 total
                                            section, Congress charges the FAA with                   ■ 1. The authority citation for part 39
                                                                                                                                                           flight cycles since installation on an airplane.
                                            promoting safe flight of civil aircraft in               continues to read as follows:                            (3) Within 500 flight cycles after the
                                            air commerce by prescribing regulations                      Authority: 49 U.S.C. 106(g), 40113, 44701.        effective date of this AD.
                                            for practices, methods, and procedures                                                                         (h) Inspection and Corrective Actions
                                                                                                     § 39.13   [Amended]
                                            the Administrator finds necessary for
                                                                                                     ■ 2. The FAA amends § 39.13 by adding                   (1) If, during any inspection required by
                                            safety in air commerce. This regulation
                                                                                                     the following new airworthiness                       paragraph (g) of this AD, any cracking of
                                            is within the scope of that authority                                                                          bracket No. 6 (P/N F2511012820000, pre-
                                            because it addresses an unsafe condition                 directive (AD):
                                                                                                                                                           modification Number 55128S18242; or P/N
                                            that is likely to exist or develop on                    2015–25–09 Airbus: Amendment 39–18347.                F2511373420000, Post-modification Number
                                            products identified in this rulemaking                       Docket No. FAA–2015–0083; Directorate             55128S18242) of the cockpit instrument
                                            action.                                                      Identifier 2014–NM–131–AD.                        panel is found, and both bracket lugs are not
                                                                                                     (a) Effective Date                                    fully broken: Within 2,600 flight cycles after
                                            Regulatory Findings                                                                                            that inspection, replace bracket No. 6 of the
                                                                                                       This AD becomes effective January 28,               cockpit instrument panel with a serviceable
                                              We determined that this AD will not                    2016.                                                 part, in accordance with the
                                            have federalism implications under                       (b) Affected ADs                                      Accomplishment Instructions of Airbus
                                            Executive Order 13132. This AD will                                                                            Service Bulletin A330–25–3538, Revision 02,
                                                                                                       None.
                                            not have a substantial direct effect on                                                                        dated April 24, 2014; or Airbus Service
                                            the States, on the relationship between                  (c) Applicability                                     Bulletin A340–25–4351, Revision 01, dated
                                            the national government and the States,                                                                        January 31, 2014; as applicable. Replacement
                                                                                                        This AD applies to the Airbus airplanes,
                                            or on the distribution of power and                                                                            of bracket No. 6 (P/N F2511012820000, pre-
                                                                                                     certificated in any category, identified in
                                                                                                                                                           modification Number 55128S18242; or P/N
                                            responsibilities among the various                       paragraphs (c)(1) and (c)(2) of this AD.
                                                                                                                                                           F2511373420000, post-modification Number
                                            levels of government.                                       (1) Model A330–201, –202, –203, –223,
                                                                                                                                                           55128S18242) of the cockpit instrument
                                                                                                     –243, –223F, –243F, –301, –302, –303, –321,
                                              For the reasons discussed above, I                     –322, –323, –341, –342, and –343 airplanes,
                                                                                                                                                           panel does not constitute terminating action
                                            certify that this AD:                                                                                          for the repetitive inspections required by
                                                                                                     all manufacturer serial numbers except those
                                                                                                                                                           paragraph (g) of this AD.
                                              1. Is not a ‘‘significant regulatory                   on which Airbus Modification 203287 has
                                                                                                                                                             (2) If, during any inspection required by
                                            action’’ under Executive Order 12866;                    been embodied in production.
                                                                                                                                                           paragraph (g) of this AD, any cracking of
                                                                                                        (2) Model A340–211, –212, –213, –311,
                                              2. Is not a ‘‘significant rule’’ under the                                                                   bracket No. 6 (P/N F2511012820000, pre-
                                                                                                     –312, and –313 airplanes, all manufacturer
                                            DOT Regulatory Policies and Procedures                                                                         modification Number 55128S18242; or P/N
                                                                                                     serial numbers.
                                            (44 FR 11034, February 26, 1979);                                                                              F2511373420000, Post-modification Number
                                                                                                     (d) Subject                                           55128S18242) of the cockpit instrument
                                              3. Will not affect intrastate aviation in                Air Transport Association (ATA) of                  panel is found and both bracket lugs are fully
                                            Alaska; and                                              America Code 25, Equipment/Furnishings.               broken: Before further flight, do a detailed
                                                                                                                                                           inspection of bracket No. 7 (P/N
                                              4. Will not have a significant                         (e) Reason                                            F2511012820000, pre-modification Number
                                            economic impact, positive or negative,                                                                         55128S18242; or P/N F2511373420000, Post-
                                                                                                        This AD was prompted by reports that a
                                            on a substantial number of small entities                                                                      modification Number 55128S18242) of the
                                                                                                     bracket that attaches the cockpit instrument
                                            under the criteria of the Regulatory                     panel to the airplane structure does not              cockpit instrument panel for cracking, in
                                            Flexibility Act.                                         sustain the fatigue loads of the design service       accordance with the Accomplishment
                                                                                                     goal. We are issuing this AD to detect and            Instructions of Airbus Service Bulletin A330–
                                            Examining the AD Docket                                                                                        25–3538, Revision 02, dated April 24, 2014;
                                                                                                     correct cracking on a bracket of the cockpit
                                                                                                     instrument panel, which, combined with                or Airbus Service Bulletin A340–25–4351,
                                              You may examine the AD docket on                                                                             Revision 01, dated January 31, 2014; as
                                            the Internet at http://                                  failure of the horizontal beam, could lead to
                                                                                                     collapse of the cockpit panel, and reduced            applicable.
                                            www.regulations.gov/                                     controllability of the airplane.                        (i) If, during the inspection required by
                                            #!docketDetail;D=FAA-2015-0083; or in                                                                          paragraph (h)(2) of this AD, no cracking is
                                            person at the Docket Management                          (f) Compliance                                        found in bracket No. 7 of the cockpit
                                            Facility between 9 a.m. and 5 p.m.,                         Comply with this AD within the                     instrument panel: Before further flight,
                                            Monday through Friday, except Federal                    compliance times specified, unless already            replace bracket No. 6 and bracket No. 7 of the
                                            holidays. The AD docket contains this                    done.                                                 cockpit instrument panel with serviceable
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                                                                                                                                                           parts, in accordance with the
                                            AD, the regulatory evaluation, any                       (g) Inspection of Bracket No. 6 of the Cockpit        Accomplishment Instructions of Airbus
                                            comments received, and other                             Instrument Panel                                      Service Bulletin A330–25–3538, Revision 02,
                                            information. The street address for the                     At the latest of the times specified in            dated April 24, 2014; or Airbus Service
                                            Docket Operations office (telephone                      paragraphs (g)(1), (g)(2), and (g)(3) of this AD:     Bulletin A340–25–4351, Revision 01, dated
                                            800–647–5527) is in the ADDRESSES                        Do a detailed inspection of bracket No. 6             January 31, 2014; as applicable. Replacement
                                            section.                                                 (part number (P/N) F2511012820000, pre-               of bracket No. 6 (P/N F2511012820000, pre-



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                                            80242            Federal Register / Vol. 80, No. 247 / Thursday, December 24, 2015 / Rules and Regulations

                                            modification Number 55128S18242; or P/N                  district office. The AMOC approval letter             National Archives and Records
                                            F2511373420000, post-modification Number                 must specifically reference this AD.                  Administration (NARA). For information on
                                            55128S18242) of the cockpit instrument                      (2) Contacting the Manufacturer: For any           the availability of this material at NARA, call
                                            panel does not constitute terminating action             requirement in this AD to obtain corrective           202–741–6030, or go to: http://
                                            for the repetitive inspections required by               actions from a manufacturer, the action must          www.archives.gov/federal-register/cfr/ibr-
                                            paragraph (g) of this AD.                                be accomplished using a method approved               locations.html.
                                              (ii) If, during the inspection required by             by the Manager, International Branch, ANM–
                                                                                                     116, Transport Airplane Directorate, FAA; or            Issued in Renton, Washington, on
                                            paragraph (h)(2) of this AD, any cracking is                                                                   December 9, 2015.
                                            found in bracket No. 7 of the cockpit                    the EASA; or Airbus’s EASA DOA. If
                                                                                                     approved by the DOA, the approval must                Michael Kaszycki,
                                            instrument panel: Although Airbus Service
                                            Bulletin A330–25–3538, Revision 02, dated                include the DOA-authorized signature.                 Acting Manager, Transport Airplane
                                            April 24, 2014; and Airbus Service Bulletin                 (3) Required for Compliance (RC): Except           Directorate, Aircraft Certification Service.
                                            A340–25–4351, Revision 01, dated January                 as required by paragraph (h)(2)(ii) of this AD,       [FR Doc. 2015–31714 Filed 12–23–15; 8:45 am]
                                            31, 2014; specify to contact Airbus for repair           if Airbus Service Bulletin A330–25–3538,
                                                                                                                                                           BILLING CODE 4910–13–P
                                            instructions, and specify that action as ‘‘RC’’          Revision 02, dated April 24, 2014; or Airbus
                                            (Required for Compliance), repair the                    Service Bulletin A340–25–4351, Revision 01,
                                                                                                     dated January 31, 2014; contain procedures
                                            cracking before further flight using a repair                                                                  DEPARTMENT OF TRANSPORTATION
                                                                                                     or tests that are identified as RC, those
                                            method approved by the Manager,
                                                                                                     procedures and tests must be done to comply
                                            International Branch, ANM–116, Transport                                                                       Federal Aviation Administration
                                                                                                     with this AD; any procedures and tests that
                                            Airplane Directorate, FAA; or the European
                                                                                                     are not identified as RC are recommended.
                                            Aviation Safety Agency (EASA); or Airbus’s
                                                                                                     Those procedures and tests that are not               14 CFR Part 39
                                            EASA Design Organization Approval (DOA).
                                                                                                     identified as RC may be deviated from, using
                                            (i) Optional Terminating Modification for                accepted methods in accordance with the               [Docket No. FAA–2015–0828; Directorate
                                            Paragraph (g) of This AD                                 operators maintenance or inspection program           Identifier 2014–NM–146–AD; Amendment
                                                                                                     without obtaining approval of an AMOC,                39–18341; AD 2015–25–03]
                                               Modifying an airplane by replacing bracket
                                                                                                     provided the procedures and tests identified
                                            No. 6 of the cockpit instrument panel with                                                                     RIN 2120–AA64
                                                                                                     as RC can be done and the airplane can be
                                            a new, reinforced bracket, in accordance with
                                                                                                     put back in an airworthy condition. Any
                                            the Accomplishment Instructions of Airbus                                                                      Airworthiness Directives; The Boeing
                                                                                                     substitutions or changes to procedures or
                                            Service Bulletin A330–25–3548, dated
                                            October 31, 2013; or Airbus Service Bulletin
                                                                                                     tests identified as RC require approval of an         Company Airplanes
                                                                                                     AMOC.
                                            A340–25–4354, dated October 31, 2013; as                                                                       AGENCY:  Federal Aviation
                                            applicable; terminates the repetitive                    (l) Related Information                               Administration (FAA), DOT.
                                            inspections required by paragraph (g) of this               (1) Refer to Mandatory Continuing
                                            AD.                                                                                                            ACTION: Final rule.
                                                                                                     Airworthiness Information (MCAI) EASA
                                            (j) Credit for Previous Actions                          Airworthiness Directive 2014–0127, dated              SUMMARY:    We are superseding
                                                                                                     May 15, 2014, for related information. This
                                               This paragraph provides credit for actions                                                                  Airworthiness Directive (AD) 2013–23–
                                                                                                     MCAI may be found in the AD docket on the
                                            required by paragraphs (g) and (h) of this AD,           Internet at http://www.regulations.gov/               03, which applies to certain The Boeing
                                            if those actions were performed before the               #!documentDetail;D=FAA-2015-0083-0002.                Company Model 747–100, 747–100B,
                                            effective date of this AD using the service                 (2) Service information identified in this         747–100B SUD, 747–200B, 747–200C,
                                            information identified in paragraph (j)(1),              AD that is not incorporated by reference is           747–200F, 747–300, 747–400, 747–
                                            (j)(2), or (j)(3) of this AD, which is not               available at the addresses specified in               400D, 747–400F, and 747SR series
                                            incorporated by reference in this AD.                    paragraphs (m)(3) and (m)(4) of this AD.
                                               (1) Airbus Service Bulletin A330–25–3538,                                                                   airplanes. AD 2013–23–03 required a
                                            dated September 10, 2013.                                (m) Material Incorporated by Reference                detailed inspection of certain attach
                                               (2) Airbus Service Bulletin A330–25–3538,                (1) The Director of the Federal Register           fittings for a cylindrical defect, and
                                            Revision 01, dated April 24, 2014.                       approved the incorporation by reference               replacement if necessary. For certain
                                               (3) Airbus Service Bulletin A340–25–4351,             (IBR) of the service information listed in this       airplanes, this new AD requires new
                                            dated September 10, 2014.                                paragraph under 5 U.S.C. 552(a) and 1 CFR             inspections of the inboard actuator
                                            (k) Other FAA AD Provisions                              part 51.                                              attach fittings for machining defects,
                                                                                                        (2) You must use this service information          and overhaul or replacement if
                                               The following provisions also apply to this           as applicable to do the actions required by
                                            AD:                                                                                                            necessary. This new AD also limits the
                                                                                                     this AD, unless this AD specifies otherwise.          compliance time for doing the
                                               (1) Alternative Methods of Compliance                    (i) Airbus Service Bulletin A330–25–3538,
                                            (AMOCs): The Manager, International                      Revision 02, dated April 24, 2014.                    replacement for certain other airplanes.
                                            Branch, ANM–116, Transport Airplane                         (ii) Airbus Service Bulletin A330–25–3548,         This AD was prompted by a report that
                                            Directorate, FAA, has the authority to                   dated October 31, 2013.                               a machining defect was also found on
                                            approve AMOCs for this AD, if requested                     (iii) Airbus Service Bulletin A340–25–             some of the actuator assemblies
                                            using the procedures found in 14 CFR 39.19.              4351, Revision 01, dated January 31, 2014.            inspected during manufacture. This
                                            In accordance with 14 CFR 39.19, send your                  (iv) Airbus Service Bulletin A340–25–              defect could lead to fatigue cracking and
                                            request to your principal inspector or local             4354, dated October 31, 2013.                         subsequent fracture. We are issuing this
                                            Flight Standards District Office, as                        (3) For service information identified in
                                            appropriate. If sending information directly                                                                   AD to detect and correct defective
                                                                                                     this AD, contact Airbus SAS, Airworthiness
                                            to the International Branch, send it to ATTN:            Office—EAL, 1 Rond Point Maurice Bellonte,            inboard actuator attach fittings which,
                                            Vladimir Ulyanov, Aerospace Engineer,                    31707 Blagnac Cedex, France; telephone +33            combined with loss of the outboard
                                            International Branch, ANM–116, Transport                 5 61 93 36 96; fax +33 5 61 93 45 80; email           actuator load path, could result in
                                            Airplane Directorate, FAA, 1601 Lind                     airworthiness.A330-A340@airbus.com;                   uncontrolled retraction of the outboard
                                            Avenue SW., Renton, WA 98057–3356;                       Internet http://www.airbus.com.                       flap, damage to flight control systems,
tkelley on DSK3SPTVN1PROD with RULES




                                            telephone 425–227–1138; fax 425–227–1149.                   (4) You may view this service information          and consequent reduced controllability
                                            Information may be emailed to: 9-ANM-116-                at the FAA, Transport Airplane Directorate,           of the airplane.
                                            AMOC-REQUESTS@faa.gov. Before using                      1601 Lind Avenue SW., Renton, WA. For
                                            any approved AMOC, notify your appropriate               information on the availability of this               DATES: This AD is effective January 28,
                                            principal inspector, or lacking a principal              material at the FAA, call 425–227–1221.               2016.
                                            inspector, the manager of the local flight                  (5) You may view this service information             The Director of the Federal Register
                                            standards district office/certificate holding            that is incorporated by reference at the              approved the incorporation by reference


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Document Created: 2015-12-24 02:24:54
Document Modified: 2015-12-24 02:24:54
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 becomes effective January 28, 2016.
ContactVladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227-1149.
FR Citation80 FR 80239 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

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