Airworthiness directives › 2021-03-11
AD 2021-03-11 Airworthiness Directives; Dassault Aviation Airplanes
Models named: FALCON 2000. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Dassault Aviation Model FALCON 2000 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 2020-02-21, with no changes. Within 90 days after March 18, 2020 (the effective date of AD 2020-02-21), revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5-40, Airworthiness Limitations, Revision 20, dated November 2018, of the Dassault Aviation Falcon 2000 Maintenance Manual. The initial compliance time for doing the tasks is at the time specified in Chapter 5-40, Airworthiness Limitations, Revision 20, dated November 2018, of the Dassault Aviation Falcon 2000 Maintenance Manual, or within 90 days after March 18, 2020, whichever occurs later, except as required by paragraphs (g)(1) through (3) of this AD. 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 date of issuance of the original airworthiness certificate or original export certificate of airworthiness. (1) For Task 30-11-09-350-801 identified in the service information specified in the introductory text of paragraph (g) of this AD, the initial compliance time is the later of the times specified in paragraphs (g)(1)(i) and (ii) of this AD. (i) At the earlier of the times specified in paragraphs (g)(1)(i)(A) and (B) of this AD. (A) Prior to the accumulation of 2,400 total flight hours or 2,000 total flight cycles, whichever occurs first. (B) Within 2,400 flight hours or 2,000 flight cycles after April 7, 2014 (the effective date of AD 2014-03-12, Amendment 39-17749 (79 FR 11693, March 3, 2014) (AD 2014-03-12)), whichever occurs first. (ii) Within 30 days after April 7, 2014 (the effective date of AD 2014-03-12). (2) For Task 52-20-00-610-801-01 identified in the service information specified in the introductory text of paragraph (g) of this AD, the initial compliance time is within 24 months after April 7, 2014 (the effective date of AD 2014-03-12). (3) The limited service life of part number F2MA721512100 is 3,750 total flight cycles on the part or 6 years since the manufacturing date of the part, whichever occurs first.
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 controllability of the airplane.
Affected ADs
(1) This AD replaces AD 2020-02-21, Amendment 39-19833 (85 FR 7860, February 12, 2020) (AD 2020-02-21). (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 →
You just looked this one up by hand
TrackAD holds all 12,278 of them and matches them against the aircraft you actually look after — airframe, engine, propeller and appliances in one pass — then works out what falls due and when.
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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