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Airworthiness directives › 2014-16-12

AD 2014-16-12 Airworthiness Directives; Dassault Aviation Airplanes

Superseded. This directive was replaced by AD 2018-19-27. Work to the current one.
2014-10-08
2014-09-03
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Airframe
2018-19-27

Models named: FALCON 2000EX. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Dassault Aviation Model FALCON 2000EX airplanes, certificated in any category, all serial numbers.

Compliance

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

Required actions

Within 30 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 9, dated February 2013, of the Dassault Falcon 2000EX Maintenance Manual. The initial compliance time for accomplishing the actions specified in Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 9, dated February 2013, of the Dassault Falcon 2000EX Maintenance Manual, is within the times specified in that maintenance manual, or 30 days after the effective date of this AD, whichever occurs later, except as provided by paragraphs (g)(1) through (g)(4) of this AD. (1) The term “landings” in the “First Inspection” column of any table in the service information means total airplane landings. (2) The term “flight hours” in the “First Inspection” column of any table in the service information means total flight hours. (3) The term “flight cycles” in the “First Inspection” column of any table in the service information means total flight cycles. (4) For task number 52-20-00-610-801-01 52-205 the initial compliance time is within 24 months after the effective date of this AD.

Unsafe condition

This AD was prompted by a revision to the airplane airworthiness limitations to introduce the corrosion prevention control program, among other changes, to the maintenance requirements and airworthiness limitations. We are issuing this AD to prevent reduced structural integrity of the airplane.

Affected ADs

Certain requirements of this AD terminate the requirements of AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010), for the airplanes identified in paragraph (c) of this AD.

Read the original on the Federal Register →

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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