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Airworthiness directives › 2014-03-12

AD 2014-03-12 Airworthiness Directives; Dassault Aviation Airplanes

Superseded. This directive was replaced by AD 2018-19-25. Work to the current one.
2014-04-07
2014-03-03
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Airframe
2018-19-25

Models named: FALCON 2000. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Dassault Aviation Model FALCON 2000 airplanes, certificated in any category, all serial numbers.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within 30 days after the effective date of this AD, revise the maintenance program to incorporate the information specified in Chapter 5-40, Airworthiness Limitations, Revision 18, dated July 2012, of Chapter 5, Maintenance Planning Document, of the Dassault Falcon 2000 Maintenance Manual. The initial compliance time for the tasks are at the applicable times specified in Chapter 5-40, Airworthiness Limitations, Revision 18, dated July 2012, of Chapter 5, Maintenance Planning Document, of the Dassault Falcon 2000 Maintenance Manual, or within 30 days after the effective date of this AD, whichever occurs later. Clarification of compliance time terminology used in the tables in the service information is provided in paragraphs (g)(1) through (g)(6) of this AD. (1) The term “landings” in the “First Inspection” column of any table in the service information specified in paragraph (g) of this AD means total airplane landings. (2) The term “flight hours” in the “First Inspection” column of any table in the service information specified in paragraph (g) of this AD means total flight hours. (3) The term “flight cycles” in the “First Inspection” column of any table in the service information specified in paragraph (g) of this AD means total flight cycles. (4) For Task 30-11-09-350-801 30-103 identified in the service information specified in paragraph (g) of this AD, the initial compliance time is the later of the times specified in paragraphs (g)(4)(i) and (g)(4)(ii) of this AD. (i) Prior to the accumulation of 2,400 total flight hours or 2,000 total flight cycles, or within 2,400 flight hours or 2,000 flight cycles after the effective date of this AD, whichever occurs first. (ii) Within 30 days after the effective date of this AD. (5) For Task 52-20-00-610-801-01 52-205 identified in the service information specified in paragraph (g) of this AD, the initial compliance time is 24 months after the effective date of this AD. (6) 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 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 prevent reduced controllability of the airplane.

Affected ADs

This AD supersedes AD 2002-23-19, Amendment 39-12963 (67 FR 71452, December 2, 2002). Certain requirements of this AD terminate certain requirements of AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 2010).

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