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Airworthiness directives › 2016-01-16

AD 2016-01-16 Airworthiness Directives; Dassault Aviation Airplanes

Superseded. This directive was replaced by AD 2017-19-03. Work to the current one.
2016-02-25
2016-01-21
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Airframe
2017-19-03

Models named: MYSTERE-FALCON 900. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to all DASSAULT AVIATION Model MYSTERE-FALCON 900 airplanes, certificated in any category.

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, Revision 20, dated October 2012, of the Dassault Aviation Falcon 900 Maintenance Manual. The initial compliance time for accomplishing the actions specified in Chapter 5-40, Airworthiness Limitations, Revision 20, dated October 2012, of the Dassault Aviation Falcon 900 Maintenance Manual, is within the applicable times specified in the maintenance manual or within 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 “LDG” in the “First Inspection” column of any table in the service information means total airplane landings. (2) The term “FH” in the “First Inspection” column of any table in the service information means total flight hours. (3) The term “FC” in the “First Inspection” column of any table in the service information means total flight cycles. (4) The term “M” in the “First Inspection” column of any table in the service information means months.

Unsafe condition

This AD was prompted by our determination of the need for a revision to the airplane airworthiness limitations to introduce a 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

This AD replaces AD 2002-23-20, Amendment 39-12964 (67 FR 71098, November 29, 2002); corrected May 4, 2010 (75 FR 23579). This AD also affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010).

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