Airworthiness directives › 2010-10-06
AD 2010-10-06 Airworthiness Directives; Airbus Model A330-200 and -300 Airplanes and Model A340-200, -300, -500, and -600 Airplanes
Models named: A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the airplanes certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 series airplanes, all serial numbers, except those on which Airbus modification 56985 has been embodied in production. (2) Airbus Model A340-211, -212, -213, -311, -312, and -313 series airplanes; and Model A340-541 and A340-642 airplanes; all serial numbers, except those on which Airbus modification 56985 has been embodied in production.
Compliance
Unless already done, do the following actions. (1) For airplanes on which the date of issuance of the original French airworthiness certificate or the date of issuance of the original French or EASA export certificate of airworthiness is before March 1, 2007: Within 63 days after June 26, 2007 (the effective date of AD 2007-12-10), in accordance with the instructions of Airbus All Operators Telex (AOT) A330-24A3042, A340-24A4056, or A340-24A5020, all Revision 02, all dated April 12, 2007; as applicable, inspect the inlet screen (last chance filter) for the generator scavenge-oil pump for signs of debris and, as applicable, apply all associated corrective actions before further flight. (2) For Model A330 aircraft operating under MMEL (master minimum equipment list) Item 24-22-01 `AC Main Generation' or MMEL Item 36-11-01 `Bleed Air Supply System Failure' and on which the date of issuance of the original French airworthiness certificate or the date of issuance of the original French or EASA export certificate of airworthiness is before March 1, 2007: As of June 26, 2007, before each flight, perform a check of the differential pressure indicator button on the lube filter and the generator scavenge filter in accordance with the instructions of Airbus AOT A330-24A3042, Revision 02, dated April 12, 2007, until accomplishment of paragraph (g)(5) of this AD. Note 1: The repetitive checks before each flight specified in paragraph (f)(2) of this AD are not required for airplanes operated under MMEL Item 36-11-01, provided the APU generator has been removed or deactivated in accordance with the instructions of Airbus AOT A330-24A3042, Revision 02, dated April 12, 2007. (3) Actions done before June 26, 2007, in accordance with the applicable Airbus service information in Table 1 of this AD are acceptable for compliance with the corresponding provisions of paragraph (f) of this AD. Table 1—Acceptable Earlier Revisions of Service Information Airbus all operators telex— Revision— Dated— A330-24A3042 Original March 22, 2007. A330-24A3042 01 March 29, 2007. A340-24A4056 Original March 22, 2007. A340-24A4056 01 March 29, 2007. A340-24A5020 Original March 22, 2007. A340-24A5020 01 March 29, 2007. RESTATEMENT OF REQUIREMENTS OF AD 2007-18-04, WITH REVISED SERVICE INFORMATION
Required actions
Unless already done, do the following actions. (1) For airplanes on which the date of issuance of the original French airworthiness certificate or the date of issuance of the original French or EASA export certificate of airworthiness is before March 1, 2007: Within 63 days after June 26, 2007 (the effective date of AD 2007-12-10), in accordance with the instructions of Airbus All Operators Telex (AOT) A330-24A3042, A340-24A4056, or A340-24A5020, all Revision 02, all dated April 12, 2007; as applicable, inspect the inlet screen (last chance filter) for the generator scavenge-oil pump for signs of debris and, as applicable, apply all associated corrective actions before further flight. (2) For Model A330 aircraft operating under MMEL (master minimum equipment list) Item 24-22-01 `AC Main Generation' or MMEL Item 36-11-01 `Bleed Air Supply System Failure' and on which the date of issuance of the original French airworthiness certificate or the date of issuance of the original French or EASA export certificate of airworthiness is before March 1, 2007: As of June 26, 2007, before each flight, perform a check of the differential pressure indicator button on the lube filter and the generator scavenge filter in accordance with the instructions of Airbus AOT A330-24A3042, Revision 02, dated April 12, 2007, until accomplishment of paragraph (g)(5) of this AD. Note 1: The repetitive checks before each flight specified in paragraph (f)(2) of this AD are not required for airplanes operated under MMEL Item 36-11-01, provided the APU generator has been removed or deactivated in accordance with the instructions of Airbus AOT A330-24A3042, Revision 02, dated April 12, 2007. (3) Actions done before June 26, 2007, in accordance with the applicable Airbus service information in Table 1 of this AD are acceptable for compliance with the corresponding provisions of paragraph (f) of this AD. Table 1—Acceptable Earlier Revisions of Service Information Airbus all operators telex— Revision— Dated— A330-24A3042 Original March 22, 2007. A330-24A3042 01 March 29, 2007. A340-24A4056 Original March 22, 2007. A340-24A4056 01 March 29, 2007. A340-24A5020 Original March 22, 2007. A340-24A5020 01 March 29, 2007. RESTATEMENT OF REQUIREMENTS OF AD 2007-18-04, WITH REVISED SERVICE INFORMATION
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1