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this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact British Aerospace
Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171, for a copy of
this service information. You may review copies at the FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington; or 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 February 5, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-2414 Filed 2-13-07; 8:45 am]
32 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-04-05 Airbus: Amendment 39-14936. Docket No. FAA-2006-26045; Directorate Identifier
2006-NM-145-AD.
Effective Date
(a) This AD becomes effective March 21, 2007.
Affected ADs
(b) This AD supersedes AD 2005-13-33.
Applicability
(c) This AD applies to Airbus A300 airplanes, all certified models and all serial numbers,
certificated in any category, except for:
(1) Airbus Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes, Model A300 B4-605R
and B4-622R airplanes, A300 F4-605R and F4-622R airplanes, and Model A300 C4-605R Variant F
airplanes.
(2) Airbus Models A300 B4-220, A300 B4-203, and A300 B2-203 airplanes in forward facing
crew cockpit certified configuration.
Unsafe Condition
(d) This AD results from the determination that repetitive operational tests are necessary
following incorporation of the wiring modification required by AD 2005-13-33. We are issuing this
AD to prevent possible trim loss when the flightcrew tries to override the autopilot pitch control,
which could result in uncontrolled flight 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 2005-13-33
Modification
(f) Within 20 months after August 1, 2005 (the effective date of AD 2005-13-33), modify the
wiring of the autopilot pitch torque limiter switch, by doing all of the applicable actions specified in
the Accomplishment Instructions of Airbus Service Bulletin A300-22-0117, dated September 7,
2004; Revision 01, dated April 20, 2005; or Revision 02, dated September 14, 2005. After the
effective date of this AD, only Revision 02 may be used.
2007-04-05 2
33 BW 2007-04
New Requirements of This AD
Repetitive Operational Tests
(g) At the applicable time specified in paragraph (g)(1) or (g)(2) of this AD: Do an operational
test of the autopilot disconnection upon pitch override, and do all applicable related investigative and
corrective actions. Do the actions in accordance with the Accomplishment Instructions of Airbus
Service Bulletin A300-22-0118, excluding Appendix 01, dated May 18, 2005; except that this AD
does not require a report of the inspection results. Do all applicable related investigative and
corrective actions before further flight. Repeat the test thereafter at intervals not to exceed 2,000
flight hours.
(1) For airplanes modified before the effective date of this AD in accordance with Airbus Service
Bulletin A300-22-0117, dated September 7, 2004: Do the initial test within 2,000 flight hours after
the effective date of this AD.
(2) For airplanes modified in accordance with Airbus Service Bulletin A300-22-0117, Revision
01, dated April 20, 2005; or Revision 02, dated September 14, 2005: Do the initial test within 2,000
flight hours after the modification required by paragraph (f) of this AD, or within 2,000 flight hours
after the effective date of this AD, whichever occurs later.
Alternative Methods of Compliance (AMOCs)
(h)(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) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the
AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate
Holding District Office.
(3) AMOCs approved previously in accordance with AD 2005-13-33 are not approved as
AMOCs with this AD.
Related Information
(i) French airworthiness directive F-2005-107, dated July 6, 2005, also addresses the subject of
this AD.
Material Incorporated by Reference
(j) You must use the service information identified in Table 1 of this AD to perform the actions
　
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