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Airworthiness directives › 2020-26-07

AD 2020-26-07 Airworthiness Directives; Dassault Aviation Airplanes

Superseded. This directive was replaced by AD 2023-04-10. Work to the current one.
2021-01-25
2020-12-21
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Airframe
2023-04-10

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

This paragraph restates the requirements of paragraph (i) of AD 2019-23-05, with no changes. Within 90 days after January 13, 2020 (the effective date of AD 2019-23-05), revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5-40, Airworthiness Limitations, Revision 24, dated September 2018, of the Dassault Aviation Falcon 900 Maintenance Manual. The initial compliance times for doing the tasks are at the times specified in Chapter 5-40, Airworthiness Limitations, Revision 24, dated September 2018, of the Dassault Aviation Falcon 900 Maintenance Manual, or within 90 days after January 13, 2020, whichever occurs later. The term “LDG” in the “First Inspection” column of any table in the service information specified in this paragraph means total airplane landings. The term “FH” in the “First Inspection” column of any table in the service information specified in this paragraph means total flight hours. The term “FC” in the “First Inspection” column of any table in the service information specified in this paragraph means total flight cycles. The term “M” in the “First Inspection” column of any table in the service information specified in this paragraph means months since the date of issuance of the original airworthiness certificate or the date of issuance of the original export certificate of airworthiness. Accomplishing the maintenance or inspection program revision required by paragraph (i) of this AD terminates the requirements of this paragraph.

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 reduced structural integrity of the airplane.

Affected ADs

(1) This AD replaces AD 2019-23-05, Amendment 39-19799 (84 FR 67169, December 9, 2019) (AD 2019-23-05). (2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010) (AD 2010-26-05).

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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