Airworthiness directives › 2014-12-02
AD 2014-12-02 Airworthiness Directives; Dassault Aviation Airplanes
Models named: FALCON F2000EX, FALCON 2000EX, FALCON 2000. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Dassault Aviation airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD; except Model FALCON F2000EX airplanes on which Dassault Aviation Modification M3254 or Dassault Service Bulletin F2000EX-300, Revision 1, dated May 17, 2013, has been embodied. (1) Model FALCON 2000EX airplanes on which Dassault Aviation modification M2846 or Dassault Aviation Technical Instruction TI-F2000EX-M2846-ME or TI-F2000EX-M3118/M2846-ME has been embodied for the installation of winglets, including the airplane having serial number 602. (2) Model FALCON 2000 and FALCON 2000EX airplanes modified by Aviation Partners Incorporated Supplemental Type Certificate (STC) ST01987SE http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/1804CCC8BA5562958625770C007757C6?OpenDocument&Highlight=st01987se (installation of winglets).
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Required actions
Within 14 days after the effective date of this AD: Revise the AFM by incorporating the CG limits identified in the service information specified in paragraph (g)(1), (g)(2), or (g)(3) of this AD, as applicable. (1) For airplanes identified in paragraph (c)(1) of this AD: Sub-sub-section 1-050-05C, “Weights; Center of gravity limits (A/C with M2846 and M3390),” Issue 2; and Sub-sub-section 1-050-05D, “Weights; Center of gravity limits (A/C with M2846 and M3000),” Issue 1; of Sub-section 1-050, “Weights and Loading,” of Section 1, “Limitations,” Issue 5, of the Dassault Aviation FALCON 2000EX EASy, FALCON 2000DX, and FALCON 2000LX AFM DGT88898, Revision 15, dated October 30, 2011. (2) For Model FALCON 2000 airplanes identified in paragraph (c)(2) of this AD: Aviation Partners, Inc. Dassault Aviation Falcon 2000 with CFE 738 Engines—Blended Winglets Installation, AFM Supplement APF2-0601, Code 002, Revision 3, dated June 1, 2012. (3) For Model FALCON 2000EX airplanes identified in paragraph (c)(2) of this AD: Aviation Partners, Inc. Dassault Aviation Falcon 2000EX Series—Blended Winglets Installation, AFM Supplement APF2-0601, Code 001, Revision 4, dated June 1, 2012.
Unsafe condition
This AD was prompted by a determination that new center of gravity (CG) limits applicable during takeoff with a Slat/Flap SF2 setting are necessary. We are issuing this AD to prevent an erratic takeoff path and consequent reduced controllability of the airplane.
Affected ADs
None.
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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