曝光台 注意防骗
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9 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-03-10 Airbus: Amendment 39-14921. Docket No. FAA-2006-24289; Directorate Identifier
2005-NM-186-AD.
Effective Date
(a) This AD becomes effective March 12, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Airbus Model A300 airplanes; A300 B4-601, B4-603, B4-620, B4-
622, B4-605R, B4-622R, A300 F4-605R, F4-622R, and C4-605R Variant F airplanes; and A310
airplanes; certificated in any category.
Unsafe Condition
(d) This AD results from fuel system reviews conducted by the manufacturer. We are issuing this
AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with
flammable fuel vapors, could result in fuel tank explosions and consequent loss 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.
Action 3–Modify the Retaining and Protection System
(f) For all airplanes identified in paragraphs (f)(1) and (f)(2) of this AD: Within 26 months after
the effective date of this AD, modify the retaining and protection system for the electrical bundles
located at the wing-to-fuselage junction, under the flap control screw jack.
(1) For Model A300 airplanes: Do the actions specified in paragraph (f) of this AD in accordance
with the Accomplishment Instructions of Airbus Service Bulletin A300-24-0085, Revision 06, dated
October 13, 2005.
(2) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, A300 F4-605R, F4-
622R, and C4-605R Variant F airplanes, except those on which Airbus Modification 10505 has been
done: Do the actions specified in paragraph (f) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300-24-6043, Revision 07, dated October 11, 2006.
2007-03-10 2
10 BW 2007-04
Action 4–Modify the Electrical Wiring of Routes 1P and 2P
(g) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, A300 F4-605R, F4-
622R, and C4-605R Variant F airplanes; except those on which Airbus Modification 11741 has been
done: Within 26 months after the effective date of this AD, modify the electrical wiring of routes 1P
and 2P (along the top panel of the shroud box and the rear spars of the wings) by extending the
protective conduits up to the next support, and replace the two existing clamps on this support with
new, improved clamps. Do all actions in accordance with the Accomplishment Instructions of Airbus
Service Bulletin A300-28-6056, Revision 01, dated January 20, 2006.
Action 5–Inspect the Wire Looms
(h) For all airplanes identified in paragraphs (h)(1) and (h)(2) of this AD: Within 26 months after
the effective date of this AD, do a general visual inspection of the wire looms on the wing trailing
edge for improperly held wires in the clamps, restore the electrical bundles to good condition, and
replace the affected nylon clamps with metallic clamps that have an elastomer lining. Do all
applicable corrective action before further flight. Repeat the inspection thereafter at intervals not to
exceed 26 months until all clamps have been replaced.
(1) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, A300 F4-605R, F4-
622R, and C4-605R Variant F airplanes; except those on which Airbus Modification 6478 has been
done: Do the actions specified in paragraph (h) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300-24-6004, Revision 04, dated November 15, 2005.
(2) For Model A310 airplanes, except those on which Airbus Modification 6478 has been done:
Do the actions specified in paragraph (h) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A310-24-2009, Revision 04, dated November 15, 2005.
Action 6–Improve the Quality of the Electrical Routes
(i) For all airplanes identified in paragraphs (i)(1), (i)(2), and (i)(3) of this AD: Within 26 months
after the effective date of this AD, replace the nylon clamps of the electrical routes in the hydraulic
compartment and in the shroud box with new metallic clamps that have white silicone lining (for
airplanes identified in paragraph (i)(1) of this AD); and/or replace the nylon clamps and change the
location of routes 1P and 2P to improve the retention of the wiring loom (for airplanes identified in
paragraphs (i)(2) and (i)(3) of this AD); as applicable.
(1) For Model A300 airplanes; except those on which Airbus Modification 11763 has been done:
Do the actions specified in paragraph (i) of this AD in accordance with the Accomplishment
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