Airworthiness directives › 2019-23-03
AD 2019-23-03 Airworthiness Directives; Dassault Aviation Airplanes
Models named: FALCON 900EX. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Dassault Aviation Model FALCON 900EX airplanes, serial number (S/N) 97 and S/Ns 120 and higher, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before September 1, 2018.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
This paragraph restates the requirements of paragraph (g) of AD 2017-19-14, with no changes. Within 90 days after October 24, 2017 (the effective date of AD 2017-19-14), revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5-40, Airworthiness Limitations, Revision 9, dated November 2015, of the Dassault Falcon 900EX EASy, Falcon 900LX, and Falcon 900DX Maintenance Manual. The initial compliance times for accomplishing the actions specified in Chapter 5-40, Airworthiness Limitations, Revision 9, dated November 2015, of the Dassault Falcon 900EX EASy, Falcon 900LX, and Falcon 900DX Maintenance Manual, is within the applicable times specified in the maintenance manual or 90 days after October 24, 2017, whichever occurs later, except as provided by paragraphs (g)(1) through (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 a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address, among other things, fatigue cracking and damage in principal structural elements; such fatigue cracking and damage could result in reduced structural integrity of the airplane.
Affected ADs
(1) This AD replaces AD 2014-16-27, Amendment 39-17951 (79 FR 51071, August 27, 2014) (“AD 2014-16-27”); and AD 2017-19-14, Amendment 39-19044 (82 FR 43674, September 19, 2017) (“AD 2017-19-14”). (2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010) (“AD 2010-26-05”).
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