Airworthiness directives › 2018-19-27
AD 2018-19-27 Airworthiness Directives; Dassault Aviation Airplanes
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, with an original certificate of airworthiness or original export certificate of airworthiness issued on or before January 15, 2018.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 90 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 11, dated November 2017, of the Dassault Falcon 2000EX Maintenance Manual. The initial compliance times for doing the tasks are at the time specified in Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 11, dated November 2017, of the Dassault Falcon 2000EX Maintenance Manual, or within 90 days after the effective date of this AD, whichever occurs later; except for task number 52-20-00-610-801-01, the initial compliance time is within 24 months after October 8, 2014 (the effective date of AD 2014-16-12). The term “LDG” in the “First Inspection” column of any table in Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 11, dated November 2017, means total airplane landings. The term “FH” in the “First Inspection” column of any table in Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 11, dated November 2017, means total flight hours. The term “FC” in the “First Inspection” column of any table in Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 11, dated November 2017, means total flight cycles.
Unsafe condition
This AD was prompted by manufacturer revisions to the airplane maintenance manual (AMM) that introduce new or more restrictive maintenance requirements and airworthiness limitations. We are issuing this AD to address reduced structural integrity of the airplane.
Affected ADs
This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010) (“AD 2010-26-05”); and AD 2014-16-12, Amendment 39-17936 (79 FR 52187, September 3, 2014) (“AD 2014-16-12”).
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