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authority. We are issuing this AD to prevent
roll oscillations during approach and landing
in certain icing, crosswind, and turbulent
conditions, which could result in reduced
controllability of the airplane.
Compliance: (e) You are responsible for
having the actions required by this AD
performed within the compliance times
specified, unless the actions have already
been done.
Restatement of Requirements of AD 2004–
03–02: Airplane Flight Manual Revision
(f) Within 10 days after February 18, 2004
(the effective date of AD 2004–03–02), revise
the Limitations section of the airplane flight
manual (AFM) to include the following
statement. This may be done by inserting a
copy of this AD into the AFM.
‘‘A321 Approach and Landing (Roll
Control) When moderate to severe icing
conditions, or significant crosswind (i.e.,
crosswinds greater than 20 knots, gust
included), or moderate to severe turbulence
are anticipated:
Use FLAP 3 for landing.’’
Note 1: When a statement identical to that
in paragraph (f) of this AD has been included
in the general revisions of the AFM, the
general revisions may be inserted into the
AFM, and the copy of this AD may be
removed from the AFM.
New Requirements of This AD: Installation
of Elevator and Aileron Computers (ELACs)
Having L83 or L91 Software
(g) Within 16 months after the effective
date of this AD: Replace existing ELACs with
ELACs having L83 software, by
accomplishing all of the actions specified in
the Accomplishment Instructions of Airbus
Service Bulletin A320–27–1151, including
Appendix 01, dated March 9, 2004; or with
ELACs having L91 software, by
accomplishing all of the actions specified in
the Accomplishment Instructions of Airbus
Service Bulletin A320–27–1152, including
Appendix 01, dated June 4, 2004; as
applicable. After accomplishing the ELAC
replacements, remove the AFM revision
required by paragraph (f) of this AD.
Accomplishing the requirements of this
paragraph terminates the requirements of
paragraph (f) of this AD.
Note 2: Airbus Service Bulletin A320–27–
1151 refers to Thales Service Bulletin
394512–27–026, dated March 5, 2004, as an
additional source of service information for
installing ELAC L83 software. Airbus Service
Bulletin A320–27–1152 refers to Thales
Service Bulletin 394512B–27–010, dated May
24, 2004, as an additional source of service
information for installing ELAC L91 software.
Concurrent Service Bulletin
(h) Prior to doing the requirements of
paragraph (g) of this AD: Install ELACs
having L81 software in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A320–27–1135, Revision 02,
dated April 18, 2002.
Previously Accomplished Actions in
Concurrent Service Bulletin
(i) Installation of ELACs having L81
software in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A320–27–1135, dated June
29, 2001; or Service Bulletin A320–27–1135,
Revision 01, dated August 31, 2001; is
acceptable for compliance with the
requirements of paragraph (h) of this AD.
Part Installation
(j) As of the effective date of this AD, no
person may install on any airplane an ELAC,
part number 3945122506, 3945123506,
3945128102, or 3945128103.
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38582 Federal Register / Vol. 70, No. 127 / Tuesday, July 5, 2005 / Rules and Regulations
Alternative Methods of Compliance
(AMOCs)
(k)(1) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
(2) Alternative methods of compliance,
approved previously in accordance with AD
2004–03–02, are approved as alternative
methods of compliance with the
corresponding requirements of this AD.
Related Information
(l) French airworthiness directive F–2004–
147, dated August 18, 2004, also addresses
the subject of this AD.
Material Incorporated by Reference
(m) You must use the service information
listed in Table 1 of this AD to perform the
actions that are required by this AD, unless
the AD specifies otherwise. The Director of
the Federal Register approves the
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