AD 2017-20-03

Within 99 months or 4,100 flight cycles, whichever occurs first, since the date of issuance of the original airworthiness certificate or date of issuance of the original export certificate of airworthiness; or within 60 days after the effective date of this AD; whichever occurs later: Do a general visual inspection of the affected electrical wiring of the airplane for worn or damaged wiring or connectors due to inadequate clearance between wiring and nearby structures, accomplish all applicable corrective actions, and modify the airplane, in accordance with the Accomplishment Instructions of Dassault Service Bulletin 7X-056, Revision 1, dated July 20, 2016, as specified in table 1 to paragraph (g) of this AD. Do all applicable corrective actions before further flight. The “Dassault service bulletin 7X-056 section” identified in table 1 to paragraph (g) of this AD is not required for airplanes on which a corresponding Dassault modification has been embodied in production, as identified in the “Excluded” column in table 1 to paragraph (g) of this AD.