[Federal Register Volume 77, Number 191 (Tuesday, October 2, 2012)]
[Proposed Rules]
[Pages 60075-60081]
[FR Doc No: 2012-24172]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-1033; Directorate Identifier 2010-NM-266-AD]
RIN 2120-AA64

Airworthiness Directives; Airbus Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to supersede an existing airworthiness directive
(AD) that applies to all Airbus Model A330-200 and -300 series
airplanes, and Model A340-200 and -300 series airplanes. The existing
AD currently requires repetitive inspections to detect discrepancies of
the transfer tubes and the collar of the ball nut of the trimmable
horizontal stabilizer actuator (THSA), and corrective action if
necessary; repetitive inspections for discrepancies of the ball screw
assembly, and corrective action if necessary; repetitive greasing of
the THSA ball nut, and replacement of the THSA if necessary; and
modification or replacement (as applicable) of the ball nut assembly,
which would end certain repetitive inspections. Since we issued that
AD, we have determined the repetitive inspections of the ball screw
assembly (and corrective action if necessary) and repetitive greasing
is needed for additional THSA nuts. This proposed AD would remove
certain inspections, revise certain actions, and add airplanes to the
applicability. We are proposing this AD to prevent degraded operation
of the THSA, which could result in reduced controllability of the
airplane.

DATES: We must receive comments on this proposed AD by November 16,
2012.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
    For Airbus service information identified in this proposed 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_ADDRESS>Internet:
http://www.airbus.com. For TRW Aeronautical Systems, SAMM Avionique,
and Lucas Aerospace service information identified in this proposed AD,
contact Goodrich Corporation, Actuation Systems, Stafford Road,
Fordhouses, Wolverhampton WV10 7EH, England; telephone +44 (0) 1902
624938; fax +44 (0) 1902 788100; email
<EMAIL_ADDRESS>Internet http://www.goodrich.com/TechPubs.Y. You may review copies of the 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>.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Operations office (telephone:<PHONE_NUMBER>) is
in the ADDRESSES section. Comments will be available in the AD docket
shortly after receipt.

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<PHONE_NUMBER>;
fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2012-1033;
Directorate Identifier 2010-NM-266-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD based on those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

    On March 17, 2005, we issued AD 2005-07-04, Amendment 39-14028 (70
FR 16104, March 30, 2005). That AD required actions intended to address
an unsafe condition on the products listed above. Since we issued AD
2005-07-04, the European Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Community, has
issued EASA Airworthiness Directive 2010-0192 (corrected), dated
October 11, 2010; and EASA Airworthiness Directive 2010-0193
(corrected), dated October 11, 2010; (referred to after this as ``the
MCAI''), to correct an unsafe condition for the specified products. The
MCAI states:

    Several cases of transfer tube disconnection from the ball-nut
of the trimmable horizontal stabilizer actuator (THSA) part number
(P/N) 47172 and 47147-400 were detected on the ground during
greasing and maintenance.
    This condition is caused by water ingress into the ball-nut
resulting in the jamming of the ball transfer circuit when the water
freezes.
    If the three (independent) ball circuits fail, then the THSA
will operate on a fail-safe nut. This nut (which operates without
balls) would then jam after several movements on the screw of the
THSA.
    This degraded operation is not detectable in the cockpit by the
crew as long as the THSA does not jam and could damage the ball
screw and the fail-safe nut.
    To detect this unsafe condition, [Direcci[oacute]n General de
Aviaci[oacute]n Civil] DGAC France AD F-2001-356 [and F-2001-357]
was issued to require repetitive inspections of the transfer tubes
and their collars in order to detect at

an early stage any distortion or initiation of disconnection.
    Further to a new case of transfer tube disconnection, * * *
[revised ADs] required an additional repetitive greasing task with
reinforcement of the ball-nut maintenance greasing instructions.
    In addition, the electrical flight control computers monitor the
operation of the THSA and the jamming of this actuator could be
detected and indicated by messages on the maintenance system and on
the [electronic centralized aircraft monitor] ECAM. In this case a
mandatory inspection of the THSA is required before the next flight.
    DGAC France AD F-2002-038 [and F-2002-037] required application
of a final fix (related to inspection and greasing task required by
DGAC France AD F-2001-356) [and F-2001-357] for the THSA P/N 47172
by application of Airbus modification 49590/Service Bulletin (SB)
A330-27-3085 [or SB A340-27-4089]. It changes the THSA P/N from
47172 to 47172-300.
    Later on, DGAC France AD F-2002-414R3 replaced the DGAC AD
France F-2001-356R2 and F-2002-038 [and DGAC France AD F2002-415R2
superseded DGAC France ADs F-2001-357R2 and F-2002-037] requiring:

--the repetitive [detailed] inspection [for discrepancies] of all
THSA P/N in service [for integrity of the primary and secondary load
path and check the Checkable Shear Pins (CSPs)], and
--the lubrication of some THSA P/N, and
--the replacement of THSA P/N 47172, 47147-400 and 47147-2XX/-3XX

    [DGAC France AD F-2002-414R3 and F-2002-415R2 correspond to FAA
AD 2005-07-04, Amendment 39-14028 (70 FR 16104, March 30, 2005).]

    Airbus has later introduced 4 new THSA P/N (47172-500, 47172-
510, 47172-520 and 47172-530).
    This [EASA] AD retains the requirements of DGAC France AD F-
2002-414R3 [and F-2002-415R2], which is superseded, and requires
repetitive inspections and lubrications of the new THSA P/N.
    The repetitive inspection and lubrication requirements for THSA
P/N 47172-520 and 47172-530 shall [also] be included in the next
Airworthiness Limitation Section (ALS) Part 4 revision.

* * * * *
    Corrective actions include replacing the THSA with a new THSA if
cracks, dents, or corrosion are found, or if the feeler gage has failed
at any of the four gaps. Corrective action is using a method approved
by either the Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA; or the EASA (or its delegated agent) for a
finding of metallic debris, loose nut, damaged or missing lock washers,
pins and parts, or incorrect installation of items. AD 2005-07-04,
Amendment 39-14028 (70 FR 16104, March 30, 2005), specified repetitive
inspections for discrepancies. This proposed AD specifies repetitive
inspections for the integrity of the primary and secondary load path,
and the CSPs, for certain airplanes. The unsafe condition is the
degraded operation of the THSA, which could result in reduced
controllability of the airplane. You may obtain further information by
examining the MCAI in the AD docket.

Relevant Service Information

    Airbus has issued the following service information for Model A330-
200 and -300 series airplanes.
     Airbus Mandatory Service Bulletin A330-27-3102, Revision
08, excluding Appendix 1, dated December 6, 2007.
     Task 27.40.00/02, Lubrication of THS Actuator Ball Screw
Nut, of Airbus A330 MRBR, Revision 12, dated July 1, 2010.
     Task<PHONE_NUMBER>1-1-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
     Task<PHONE_NUMBER>1-1-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
     Task<PHONE_NUMBER>1-2-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
     Task<PHONE_NUMBER>1-2-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
     Task<PHONE_NUMBER>1-3-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
     Task<PHONE_NUMBER>1-3-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
     Task<PHONE_NUMBER>1-4-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
     Task<PHONE_NUMBER>1-4-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
     Task<PHONE_NUMBER>2-1-E, Lubrication of the THSA Ball Nut,
of Airbus A330 ALS Part 4--Ageing Systems Maintenance, Revision 02,
dated December 16, 2009.
    Airbus has issued the following service information for Model A340-
200 and -300 series airplanes.
     Airbus Mandatory Service Bulletin A340-27-4107, Revision
08, excluding Appendix 1, dated December 6, 2007.
     Task 27.40.00/02, Lubrication of THS Actuator Ball Screw
Nut, of Airbus A340 MRBR, Revision 12, dated July 1, 2010.
     Task<PHONE_NUMBER>1-1-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
     Task<PHONE_NUMBER>1-1-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
     Task<PHONE_NUMBER>1-2-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
     Task<PHONE_NUMBER>1-2-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
     Task<PHONE_NUMBER>1-3-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
     Task<PHONE_NUMBER>1-3-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
     Task<PHONE_NUMBER>1-4-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
     Task<PHONE_NUMBER>1-4-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
     Task<PHONE_NUMBER>2-1-E, Lubrication of the THSA Ball Nut,
of Airbus of A340 ALS Part 4--Ageing Systems Maintenance, Revision 01,
dated December 15, 2009.
    The actions described in this service information are intended to
correct the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of This Proposed AD

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

Explanation of Updated Credit Language

    We have revised the heading and wording for paragraph (i) of this
AD to provide appropriate credit for previous accomplishment of certain
actions. This change does not affect the intent of that paragraph.

Explanation of Change to Costs of Compliance

    Since issuance of AD 2005-07-04, Amendment 39-14028 (70 FR 16104,

March 30, 2005), we have increased the labor rate used in the Costs of
Compliance from $65 per work-hour to $85 per work-hour. The Costs of
Compliance information, below, reflects this increase in the specified
labor rate.

Costs of Compliance

    Based on the service information, we estimate that this proposed AD
would affect about 33 products of U.S. registry.
    The actions that are required by AD 2005-07-04, Amendment 39-14028
(70 FR 16104, March 30, 2005), and retained in this proposed AD take up
to 36 work-hours per product, at an average labor rate of $85 per work
hour. Based on these figures, the estimated cost of the currently
required actions is up to $3,060 per product.
    We estimate that it would take about 2 work-hours per product to
comply with the new basic requirements of this proposed AD. The average
labor rate is $85 per work-hour. Based on these figures, we estimate
the cost of the proposed AD on U.S. operators to be $5,610, or $170 per
product.
    We have received no definitive data that would enable us to provide
cost estimates for the on-condition actions specified in this proposed
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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed
regulation:
    1. Is not a ``significant regulatory action'' under Executive Order
12866,
    2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
    3. Will not affect intrastate aviation in Alaska, and
    4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to
comply with this proposed AD and placed it in the AD docket.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

    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]

    2. The FAA amends Sec.  39.13 by removing AD 2005-07-04, Amendment
39-14028 (70 FR 16104, March 30, 2005), and adding the following new
AD:

Airbus: Docket No. FAA-2012-1033; Directorate Identifier 2010-NM-
266-AD.

(a) Comments Due Date

    We must receive comments by November 16, 2012.

(b) Affected ADs

    This AD supersedes AD 2005-07-04, Amendment 39-14028 (70 FR
16104, March 30, 2005).

(c) Applicability

    This AD applies to all Airbus Model A330-201, -202, -203, -223,
-223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342,
and -343 airplanes; and Model A340-211, -212, -213, -311, -312, and
-313 airplanes; certificated in any category.

(d) Subject

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

(e) Reason

    This AD was prompted by several reports of disconnection of the
transfer tube from the ball nut of the trimmable horizontal
stabilizer actuator (THSA). We are issuing this AD to prevent
degraded operation of the THSA, which could result in reduced
controllability of the airplane.

(f) Compliance

    You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.

(g) Retained Modification or Replacement

    This paragraph restates the requirements of paragraph (g) of AD
2005-07-04, Amendment 39-14028 (70 FR 16104, March 30, 2005). Except
for Model A330-223F and -243F airplanes: Within 24 months after May
4, 2005 (the effective date of AD 2005-07-04), modify the ball nut
of each THSA by doing paragraph (g)(1) or (g)(2) of this AD, as
applicable.
    (1) For THSAs having P/N 47172: Modify the ball nut of the THSA,
or replace the existing THSA with a serviceable part having P/N
47172-300; in accordance with Airbus Service Bulletin A330-27-3085
(for Model A330 series airplanes) or A340-27-4089 (for Model A340-
313 series airplanes), both Revision 02, both dated September 5,
2002; as applicable.

    Note 1 to paragraph (g)(1) of this AD:  Airbus Service Bulletins
A330-27-3085 and A340-27-4089, both Revision 02, both dated
September 5, 2002, refer to TRW Aeronautical Systems Service
Bulletin 47172-27-03, dated October 24, 2001, which is not
incorporated by reference in this AD, as additional guidance for
accomplishing the modification of the ball nut of the THSA.

    (2) For THSAs having P/N 47147-200, -210, -213, -300, -303, -
350, or -400: Modify the ball nut of the THSA, or replace the
existing THSA with an improved part having P/N 47147-500; as
applicable; in accordance with Airbus Service Bulletin A330-27-3093
(for Model A330 series airplanes) or A340-27-4099 (for Model A340-
200 and -300 series airplanes), both Revision 01, both dated
September 5, 2002; as applicable.

    Note 2 to paragraph (g)(2) of this AD:  Airbus Service Bulletins
A330-27-3093 and A340-27-4099, both Revision 01, both dated
September 5, 2002, refer to TRW Aeronautical Systems Service
Bulletin 47147-27-10, dated June 27, 2002, which is not incorporated
by reference in this AD, as additional guidance for accomplishing
the modification of the ball nut of the THSA.

(h) Retained Previous/Concurrent Requirements

    This paragraph restates the requirements of paragraph (h) of AD
2005-07-04, Amendment 39-14028 (70 FR 16104, March 30, 2005).
    (1) Except for Model A330-223F and -243F airplanes, prior to or
concurrently with accomplishing the requirements of paragraph (g)(2)
of this AD, do all of the actions specified in the Accomplishment
Instructions of the applicable Airbus service bulletins listed in
table 1 or 2 to paragraph (h)(1) of this AD, as applicable, in
accordance with those service bulletins.

    Note 3 to paragraph (h)(1) of this AD:  Airbus Service Bulletin
A330-27-3093,

Revision 01, dated September 5, 2002, specifies that the actions in
Airbus Service Bulletin A330-27-3052 be accomplished previously or
concurrently. Airbus Service Bulletin A330-27-3052, Revision 03,
dated December 5, 2001, specifies that the actions in Airbus Service
Bulletins A330-27-3007, A330-27-3015, A330-27-3047, A330-27-3050,
and A330-55-3020 be accomplished previously or concurrently.

    Note 4 to paragraph (h)(1) of this AD:  Airbus Service Bulletin
A340-27-4099, Revision 01, dated September 5, 2002, specifies that
the actions in Airbus Service Bulletin A340-27-4059 be accomplished
previously or concurrently. Airbus Service Bulletin A340-27-4059,
Revision 03, dated December 5, 2001, specifies that the actions in
Airbus Service Bulletins A340-27-4007, A340-27-4025, A340-27-4054,
A340-27-4057, and A340-55-4021 be accomplished previously or
concurrently.

     Table 1 to Paragraph (h)(1) of This AD--Retained Previous/Concurrent Requirements for Model A330 Series
                                                    Airplanes
----------------------------------------------------------------------------------------------------------------
                                                                                Additional source of
                                                                                guidance  (not
   Airbus service bulletin--      Revision        Date--             Main action--           incorporated by
                                  level--                                                reference  in this AD)--

----------------------------------------------------------------------------------------------------------------
A330-27-3007...................         01  September 18, 1996  Replace rudder servo     Samm Avionique Service
                                                                 controls with modified   Bulletin SC5300-27-24-
                                                                 parts.                   01, dated April 15,
                                                                                1994.
A330-27-3015...................  .........  June 7, 1995......  Modify the control       Lucas Aerospace Service
                                                                 valve detent and the     Bulletin 47147-27-02,
                                                                 jamming protection       Revision 1, dated
                                                                 device on the THSA.      January 31, 1996.
A330-27-3047...................         01  November 26, 1997.  Replace hydraulic        Lucas Aerospace Service
                                                                 motors on the THSA       Bulletin 47147-27-04,
                                                                 with new parts.          Revision 1, dated June
                                                                                20, 1997.
A330-27-3050...................  .........  November 15, 1996.  Replace mechanical       Lucas Aerospace Service
                                                                 input shaft for THSA     Bulletin 47147-27-05,
                                                                 with modified part.      dated November 8,
                                                                                1996.
A330-27-3052...................         03  December 5, 2001..  Replace THSA with a      Lucas Aerospace Service
                                                                 modified THSA.           Bulletin 47147-27-07,
                                                                                dated May 4, 1998.
A330-55-3020...................         01  October 21, 1998..  Perform a general        None.
                                                                 visual inspection of
                                                                 the THSA screw jack
                                                                 fitting assembly for
                                                                 correct installation
                                                                 of a washer; and
                                                                 correctly install
                                                                 washer as applicable.
----------------------------------------------------------------------------------------------------------------

     Table 2 to Paragraph (h)(1) of This AD--Retained Previous/Concurrent Requirements for Model A340 Series
                                                    Airplanes
----------------------------------------------------------------------------------------------------------------
                                                                                Additional source of
                                                                                guidance  (not
   Airbus service bulletin--      Revision        Date--             Main action--           incorporated by
                                  level--                                                reference  in this AD)--

----------------------------------------------------------------------------------------------------------------
A340-27-4007...................  .........  April 7, 1994.....  Replace hydraulic        Lucas Aerospace Service
                                                                 motors on the THSA       Bulletin 47147-27-01,
                                                                 with new parts.          dated May 4, 1998.
A340-27-4025...................  .........  June 7, 1995......  Modify the control       Lucas Aerospace Service
                                                                 valve detent and the     Bulletin 47147-27-02,
                                                                 jamming protection       Revision 1, dated
                                                                 device on the THSA.      January 31, 1996.
A340-27-4054...................         01  November 26, 1997.  Replace hydraulic        Lucas Aerospace Service
                                                                 motors on the THSA       Bulletin 47147-27-04,
                                                                 with new parts.          Revision 1, dated June
                                                                                20, 1997.
A340-27-4057...................  .........  November 15, 1996.  Replace mechanical       Lucas Aerospace Service
                                                                 input shaft for THSA     Bulletin 47147-27-05,
                                                                 with modified part.      dated November 8,
                                                                                1996.
A340-27-4059...................         03  December 5, 2001..  Replace THSA with a      Lucas Aerospace Service
                                                                 modified THSA.           Bulletin 47147-27-07,
                                                                                dated May 4, 1998.
A340-55-4021...................         01  October 21, 1998..  Perform a general        None.
                                                                 visual inspection of
                                                                 the THSA screw jack
                                                                 fitting assembly for
                                                                 correct installation
                                                                 of a washer; and
                                                                 correctly install
                                                                 washer as applicable.
----------------------------------------------------------------------------------------------------------------

    (2) For the purposes of this AD, a general visual inspection is:
``A visual examination of an interior or exterior area,
installation, or assembly to detect obvious damage, failure, or
irregularity. This level of inspection is made from within touching
distance unless otherwise specified. A mirror may be necessary to
ensure visual access to all surfaces in the inspection area. This
level of inspection is made under normally available lighting
conditions such as daylight, hangar lighting, flashlight, or
droplight and may require removal or opening of access panels or
doors. Stands, ladders, or platforms may be required to gain
proximity to the area being checked.''

(i) Retained Credit for Previous Actions

    This paragraph provides credit for the actions specified in
paragraphs (i)(1) and (i)(2) of this AD.
    (1) This paragraph provides credit for the requirements of
paragraph (g)(1) of this AD, if those actions were performed before
May 4, 2005 (the effective date of AD 2005-07-04, Amendment 39-14028
(70 FR 16104, March 30, 2005)), using Airbus Service Bulletin A330-
27-3085 (for Model A330 series airplanes) or A340-27-4089 (for Model
A340-313 series airplanes), both Revision 01, both dated January 23,
2002 (which are not incorporated by reference in this AD), as
applicable.
    (2) This paragraph provides credit for the requirements of
paragraphs (g)(2) of this AD, if those actions were performed before
May 4, 2005 (the effective date of AD 2005-07-04, Amendment 39-14028
(70 FR 16104, March 30, 2005)), using Airbus Service Bulletin A330-
27-3093 (for Model A330 series airplanes) or A340-27-4099 (for Model
A340-200 and -300 series airplanes), both dated June 27, 2002 (which
are not incorporated by reference in this AD), as applicable.

(j) New Repetitive Greasing Procedure

    (1) Within 700 flight hours after the effective date of this AD
or within 700 flight

hours after the date of the last lubrication, whichever occurs
later, and thereafter at intervals not to exceed 700 flight hours
from the last lubrication of the trimmable horizontal stabilizer
(THS) actuator ball screw nut: Perform Task 27.40.00/02, Lubrication
of THS Actuator Ball Screw Nut, in accordance with Airbus A330
Maintenance Review Board Report (MRBR), Revision 12, dated July 1,
2010 (for Model A330 series airplanes); or Airbus A340 MRBR,
Revision 12, dated July 1, 2010 (for Model A340 series airplanes);
on all THSA.
    (2) For airplanes identified in paragraphs (j)(2)(i),
(j)(2)(ii), and (j)(2)(iii) of this AD, as applicable, lubrication
of the THS actuator ball screw nut performed at threshold and
repetitive interval not exceeding 1,000 flight hours, in accordance
with Task<PHONE_NUMBER>2-1-E, Lubrication of the THSA Ball Nut, of
Airbus A330 Airworthiness Limitations Section (ALS) Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009 (for Model
A330 series airplanes); or Task<PHONE_NUMBER>2-1-E, Lubrication of the
THSA Ball Nut, of Airbus of A340 ALS Part 4--Ageing Systems
Maintenance, Revision 01, dated December 15, 2009 (for Model A340-
200 and -300 series airplanes); is acceptable for compliance with
requirements of paragraph (j)(1) of this AD.
    (i) Airplanes on which Airbus Modifications 52269, 56056, and
55780 have been done in production.
    (ii) Model A330 series airplanes on which the actions specified
in Airbus Mandatory Service Bulletin A330-27-3137, dated March 20,
2007, Revision 01, dated December 6, 2007, or Revision 02, dated
January 18, 2010; and Airbus Mandatory Service Bulletin A330-92-
3046, Revision 04, dated July 16, 2010, or Revision 05, dated
November 7, 2011; (which are not incorporated by reference in this
AD) have been done in service.
    (iii) Model A340-200 and -300 series airplanes on which the
actions specified in Airbus Mandatory Service Bulletin A340-27-4136,
dated March 20, 2007, Revision 01, dated December 6, 2007, or
Revision 02, dated February 24, 2010; and Airbus Mandatory Service
Bulletin A340-92-4056, Revision 03, dated July 16, 2010; (which are
not incorporated by reference in this AD) have been done in service.

(k) New Repetitive Inspections of the Ball Screw Assembly and
Corrective Actions

    For all airplanes, except for those airplanes identified in
paragraphs (k)(1), (k)(2), and (k)(3) of this AD: Do the applicable
actions specified in paragraphs (k)(4) and (k)(5) of this AD within
700 flight hours after the effective date of this AD, and repeat the
inspection thereafter at intervals not to exceed 700 flight hours.
    (1) Airplanes on which the actions specified in Airbus
Modifications 52269, 56056, and 55780 have been done in production.
    (2) Model A330 series airplanes on which Airbus Mandatory
Service Bulletin A330-27-3137, dated March 20, 2007, Revision 01,
dated December 6, 2007, or Revision 02, dated January 18, 2010; and
Airbus Mandatory Service Bulletin A330-92-3046, Revision 04, dated
July 16, 2010, or Revision 05, dated November 7, 2011; (which are
not incorporated by reference in this AD) have been done in service.
    (3) Model A340-200 and -300 series airplanes on which the
actions specified in Airbus Mandatory Service Bulletin A340-27-4136,
dated March 20, 2007, Revision 01, dated December 6, 2007, or
Revision 02, dated February 24, 2010; and Airbus Mandatory Service
Bulletin A340-92-4056, Revision 03, dated July 16, 2010; have been
done in service.
    (4) For airplanes on which the actions specified in Airbus
Mandatory Service Bulletin A330-27-3137, dated March 20, 2007,
Revision 01, dated December 6, 2007, or Revision 02, dated January
18, 2010 (for Model A330 series airplanes); or Airbus Mandatory
Service Bulletin A340-27-4136, dated March 20, 2007, Revision 01,
dated December 6, 2007, or Revision 02, dated February 24, 2010 (for
Model A340-200 and -300 series airplanes); (which are not
incorporated by reference in this AD) have been done: Do the
applicable detailed inspection of the ball screw assembly for
integrity of the primary and secondary load path and check the
checkable shear pins (CSP), and do all applicable corrective
actions, in accordance with the Accomplishment Instructions of
Airbus Mandatory Service Bulletin A330-27-3102, Revision 08,
excluding Appendix 1, dated December 6, 2007 (for Model A330 series
airplanes); or Airbus Mandatory Service Bulletin A340-27-4107,
Revision 08, excluding Appendix 1, dated December 6, 2007 (for Model
A340-200 and -300 series airplanes); except as required by paragraph
(k)(6) of this AD. Do all applicable corrective actions before
further flight.
    (5) For airplanes on which the actions specified in Airbus
Mandatory Service Bulletin A330-27-3137, dated March 20, 2007,
Revision 01, dated December 6, 2007, or Revision 02, dated January
18, 2010 (for Model A330 series airplanes); or Airbus Mandatory
Service Bulletin A340-27-4136, dated March 20, 2007, Revision 01,
dated December 6, 2007, or Revision 02, dated February 24, 2010 (for
Model A340-200 and -300 series airplanes); (which are not
incorporated by reference in this AD) have not been done: Perform a
detailed inspection of the ball screw assembly for integrity of the
primary and secondary load path, and do all applicable corrective
actions, in accordance with the Accomplishment Instructions of
Airbus Mandatory Service Bulletin A330-27-3102, Revision 08,
excluding Appendix 1, dated December 6, 2007 (for Model A330 series
airplanes); or Airbus Mandatory Service Bulletin A340-27-4107,
Revision 08, excluding Appendix 1, dated December 6, 2007 (for Model
A340 series airplanes); except as required by paragraph (k)(6) of
this AD. Do all applicable corrective actions before further flight.
    (6) Where Airbus Mandatory Service Bulletin A330-27-3102,
Revision 08, excluding Appendix 1, dated December 6, 2007 (for Model
A330 series airplanes); or Airbus Mandatory Service Bulletin A340-
27-4107, Revision 08, excluding Appendix 1, dated December 6, 2007
(for Model A340 series airplanes); specify contacting Airbus for a
damage assessment, this AD requires contacting the Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA;
or the European Aviation Safety Agency (EASA) (or its delegated
agent); for required actions before further flight, and doing the
specified actions within the times given.

(l) New Actions for Electronic Centralized Aircraft Monitor (ECAM)
Fault Messages

    For airplanes identified in paragraph (k) of this AD, if one of
the ``PRIM X PITCH FAULT'' or ``STAB CTL FAULT'' messages is
displayed on the ECAM associated with the ``PITCH TRIM ACTR (1CS)''
maintenance message, do the applicable detailed inspection and all
applicable corrective actions specified in paragraph (k)(4) or
(k)(5) of this AD, as applicable to airplane configuration, before
further flight after the message is displayed on the ECAM.

(m) New Optional Method of Compliance

    For airplanes having THSA P/N 47147-500, 47147-700, 47172-300,
47172-500, or 47172-510, accomplishing the repetitive actions
specified in paragraph (m)(1) or (m)(2) of this AD, as applicable,
is acceptable for compliance with the corresponding actions
specified in paragraph (k)(4) or (k)(5) of this AD, as applicable.
    (1) For Model A330 series airplanes, the repetitive actions
specified in paragraphs (m)(1)(i) through (m)(1)(viii) of this AD.
    (i) Task<PHONE_NUMBER>1-1-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (ii) Task<PHONE_NUMBER>1-1-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (iii) Task<PHONE_NUMBER>1-2-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (iv) Task<PHONE_NUMBER>1-2-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (v) Task<PHONE_NUMBER>1-3-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (vi) Task<PHONE_NUMBER>1-3-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (vii) Task<PHONE_NUMBER>1-4-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (viii) Task<PHONE_NUMBER>1-4-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (2) For Model A340-200 and -300 series airplanes, the repetitive
actions specified in paragraphs (m)(2)(i) through (m)(2)(viii) of
this AD.
    (i) Task<PHONE_NUMBER>1-1-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (ii) Task<PHONE_NUMBER>1-1-E of Airbus A340 ALS Part 4--Ageing
Systems

Maintenance, Revision 02, dated October 12, 2011.
    (iii) Task<PHONE_NUMBER>1-2-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (iv) Task<PHONE_NUMBER>1-2-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
    (v) Task<PHONE_NUMBER>1-3-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (vi) Task<PHONE_NUMBER>1-3-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
    (vii) Task<PHONE_NUMBER>1-4-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (viii) Task<PHONE_NUMBER>1-4-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.

(n) New Credit for Previous Actions

    (1) This paragraph provides credit for the inspections and
corrective actions required by paragraph (k) of this AD, if those
actions were performed before the effective date of this AD using
the service information specified in paragraphs (n)(1)(i) through
(n)(1)(vi) of this AD (which is not incorporated by reference in
this AD).
    (i) Airbus Service Bulletin A330-27-3102, Revision 02, excluding
Appendix 01, dated November 7, 2002.
    (ii) Airbus Service Bulletin A330-27-3102, Revision 03,
excluding Appendix 01, dated June 20, 2003.
    (iii) Airbus Service Bulletin A330-27-3102, Revision 04,
excluding Appendix 01, dated December 8, 2003.
    (iv) Airbus Mandatory Service Bulletin A330-27-3102, Revision
05, excluding Appendix 01, dated July 7, 2004.
    (v) Airbus Mandatory Service Bulletin A330-27-3102, Revision 06,
excluding Appendix 01, dated December 16, 2005.
    (vi) Airbus Mandatory Service Bulletin A330-27-3102, Revision
07, excluding Appendix 01, dated March 16, 2007.
    (2) This paragraph provides credit for the inspections and
corrective actions required by paragraph (k) of this AD, if those
actions were performed before the effective date of this AD using
the service information specified in paragraphs (n)(2)(i) through
(n)(2)(vi) of this AD (which is not incorporated by reference in
this AD).
    (i) Airbus Service Bulletin A340-27-4107, Revision 02, excluding
Appendix 01, dated September 23, 2002.
    (ii) Airbus Service Bulletin A340-27-4107, Revision 03,
excluding Appendix 01, dated December 4, 2002.
    (iii) Airbus Mandatory Service Bulletin A340-27-4107, Revision
04, excluding Appendix 01, dated June 20, 2003.
    (iv) Airbus Mandatory Service Bulletin A340-27-4107, Revision
05, excluding Appendix 01, dated December 8, 2003.
    (v) Airbus Mandatory Service Bulletin A340-27-4107, Revision 06,
excluding Appendix 01, dated December 16, 2005.
    (vi) Airbus Mandatory Service Bulletin A340-27-4107, Revision
07, excluding Appendix 01, dated March 16, 2007.
    (3) This paragraph provides credit for the actions specified in
paragraph (j) of this AD, if those actions were performed before the
effective date of this AD using Task 27.40.00/02, Lubrication of THS
Actuator Ball Screw Nut, of Airbus A330 MRBR, Revision 11, dated
June 18, 2008 (which is not incorporated by reference in this AD).
    (4) This paragraph provides credit for the actions specified in
paragraph (j) of this AD, if those actions were performed before the
effective date of this AD using Task 27.40.00/02, Lubrication of THS
Actuator Ball Screw Nut, of Airbus A340 MRBR, Revision 11, dated
June 18, 2008 (which is not incorporated by reference in this AD).

(o) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, 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:<PHONE_NUMBER>. Information may be emailed to<EMAIL_ADDRESS>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) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.

(p) Related Information

    (1) Refer to MCAI EASA Airworthiness Directive 2010-0192
(corrected), dated October 11, 2010; EASA Airworthiness Directive
2010-0193 (corrected), dated October 11, 2010; and the following
service information; for related information
    (i) Airbus Mandatory Service Bulletin A330-27-3102, Revision 08,
excluding Appendix 1, dated December 6, 2007.
    (ii) Airbus Mandatory Service Bulletin A340-27-4107, Revision
08, excluding Appendix 1, dated December 6, 2007.
    (iii) Airbus Service Bulletin A330-27-3007, Revision 01, dated
September 18, 1996.
    (iv) Airbus Service Bulletin A330-27-3015, dated June 7, 1995.
    (v) Airbus Service Bulletin A330-27-3047, Revision 01, dated
November 26, 1997.
    (vi) Airbus Service Bulletin A330-27-3050, dated November 15,
1996.
    (vii) Airbus Service Bulletin A330-27-3052, Revision 03, dated
December 5, 2001.
    (viii) Airbus Service Bulletin A330-27-3085, Revision 02, dated
September 5, 2002.
    (ix) Airbus Service Bulletin A330-27-3093, Revision 01, dated
September 5, 2002.
    (x) Airbus Service Bulletin A330-55-3020, Revision 01, dated
October 21, 1998.
    (xi) Airbus Service Bulletin A340-27-4007, dated April 7, 1994.
    (xii) Airbus Service Bulletin A340-27-4025, dated June 7, 1995.
    (xiii) Airbus Service Bulletin A340-27-4054, Revision 01, dated
November 26, 1997.
    (xiv) Airbus Service Bulletin A340-27-4057, dated November 15,
1996.
    (xv) Airbus Service Bulletin A340-27-4059, Revision 03, dated
December 5, 2001.
    (xvi) Airbus Service Bulletin A340-27-4089, Revision 02, dated
September 5, 2002.
    (xvii) Airbus Service Bulletin A340-27-4099, Revision 01, dated
September 5, 2002.
    (xviii) Airbus Service Bulletin A340-55-4021, Revision 01,
October 21, 1998.
    (xix) Task 27.40.00/02, Lubrication of THS Actuator Ball Screw
Nut, of Airbus A330 MRBR, Revision 12, dated July 1, 2010.
    (xx) Task 27.40.00/02, Lubrication of THS Actuator Ball Screw
Nut, of Airbus A340 MRBR, Revision 12, dated July 1, 2010.
    (xxi) Task<PHONE_NUMBER>1-1-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (xxii) Task<PHONE_NUMBER>1-1-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (xxiii) Task<PHONE_NUMBER>1-1-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (xxiv) Task<PHONE_NUMBER>1-1-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
    (xxv) Task<PHONE_NUMBER>1-2-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (xxvi) Task<PHONE_NUMBER>1-2-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (xxvii) Task<PHONE_NUMBER>1-2-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (xxviii) Task<PHONE_NUMBER>1-2-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
    (xxix) Task<PHONE_NUMBER>1-3-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (xxx) Task<PHONE_NUMBER>1-3-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (xxxi) Task<PHONE_NUMBER>1-3-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.

    (xxxii) Task<PHONE_NUMBER>1-3-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
    (xxxiii) Task<PHONE_NUMBER>1-4-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated December 16, 2009.
    (xxxiv) Task<PHONE_NUMBER>1-4-E of Airbus A330 ALS Part 4--Ageing
Systems Maintenance, Revision 03, dated September 9, 2011.
    (xxxv) Task<PHONE_NUMBER>1-4-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 01, dated December 15, 2009.
    (xxxvi) Task<PHONE_NUMBER>1-4-E of Airbus A340 ALS Part 4--Ageing
Systems Maintenance, Revision 02, dated October 12, 2011.
    (xxxvii) Task<PHONE_NUMBER>2-1-E, Lubrication of the THSA Ball
Nut, of Airbus A330 ALS Part 4--Ageing Systems Maintenance, Revision
02, dated December 16, 2009.
    (xxxviii) Task<PHONE_NUMBER>2-1-E, Lubrication of the THSA Ball
Nut, of Airbus of A340 ALS Part 4--Ageing Systems Maintenance,
Revision 01, dated December 15, 2009.
    (2) For Airbus 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_ADDRESS>
Internet: http://www.airbus.com. For TRW Aeronautical Systems, SAMM
Avionique, and Lucas Aerospace service information identified in
this proposed AD, contact Goodrich Corporation, Actuation Systems,
Stafford Road, Fordhouses, Wolverhampton WV10 7EH, England;
telephone +44 (0) 1902 624938; fax +44 (0) 1902 788100; email
<EMAIL_ADDRESS>Internet http://www.goodrich.com/TechPubs.Y. You may review copies of the 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>.

    Issued in Renton, Washington, on September 21, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-24172 Filed 10-1-12; 8:45 am]
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