TrackAD

Airworthiness directives › 2015-16-02

AD 2015-16-02 Airworthiness Directives; Airbus Airplanes

Superseded. This directive was replaced by AD 2017-05-10. Work to the current one.
2015-09-15
2015-08-11
—
—
Airframe
2017-05-10

Models named: A330-201, -202, -203, -223, -243, -223F, -243F, -301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus Model A330-201, -202, -203, -223, -243, -223F, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes; certificated in any category; all manufacturer serial numbers.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within 6 months after the effective date of this AD, revise the maintenance program or inspection program, as applicable, by incorporating Airbus A330 Airworthiness Limitations Section (ALS) Part 4—Aging Systems Maintenance, Revision 04, dated August 27, 2013, and Airbus A330 ALS Part 4—Aging Systems Maintenance (ASM), Variation 4.1 and Variation 4.2, both dated July 23, 2014. The initial compliance times for the actions are within the applicable compliance times specified in the Record of Revisions pages of Airbus A330 ALS Part 4—Aging Systems Maintenance, Revision 04, dated August 27, 2013, Airbus A330 ALS Part 4—Aging Systems Maintenance (ASM), Variation 4.1 and Variation 4.2, both dated July 23, 2014, or within 6 months after the effective date of this AD, whichever is later, except as required by paragraph (h) of this AD.

Unsafe condition

This AD was prompted by a determination that more restrictive maintenance requirements and airworthiness limitations are necessary. We are issuing this AD to address the aging effects of aircraft systems. Such aging effects could change the characteristics of those systems, which, in isolation or in combination with one or more other specific failures or events, could result in failure of certain life limited parts, which could reduce the structural integrity of the airplane or reduce the controllability of the airplane.

Affected ADs

This AD replaces the ADs specified in paragraphs (b)(1) through (b)(9) of this AD. (1) AD 2003-14-11, Amendment 39-13230 (68 FR 41521, July 14, 2003). (2) AD 2004-11-08, Amendment 39-13654 (69 FR 31874, June 8, 2004). (3) AD 2004-13-25, Amendment 39-13707 (69 FR 41394, July 9, 2004). (4) AD 2004-18-14, Amendment 39-13793 (69 FR 55326, September 14, 2004). (5) AD 2007-05-12, Amendment 39-14973 (72 FR 10057, March 7, 2007). (6) AD 2008-06-07, Amendment 39-15419 (73 FR 13103, March 12, 2008; corrected April 15, 2008 (73 FR 20367)). (7) AD 2009-18-20, Amendment 39-16017 (74 FR 46313, September 9, 2009). (8) AD 2010-15-02, Amendment 39-16368 (75 FR 42589, July 22, 2010). (9) AD 2012-04-07, Amendment 39-16963 (77 FR 12989, March 5, 2012).

Read the original on the Federal Register →

You just looked this one up by hand

TrackAD holds all 12,278 of them and matches them against the aircraft you actually look after — airframe, engine, propeller and appliances in one pass — then works out what falls due and when.

Look round a real shop first Start free

The demonstration shop is eleven real aircraft with a year of work behind them. No account needed.

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