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Airworthiness directives › 2016-10-16

AD 2016-10-16 Airworthiness Directives; Dassault Aviation Airplanes

2016-06-27
2016-05-23
39-18527
FAA-2015-8426
Airframe
—

Models named: MYSTERE-FALCON 900, FALCON 900EX, FALCON 2000EX. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to the airplanes specified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category. (1) Dassault Aviation Model MYSTERE-FALCON 900 airplanes, all serial numbers. (2) Dassault Aviation Model FALCON 900EX airplanes, all serial numbers, except airplanes with “EASy II” “2nd certification” avionics, which are defined as: Airplanes modified in production with Dassault Aviation modification M5595; or airplanes modified in service with Dassault Aviation Service Bulletin F900EX-400 or with Dassault Aviation Service Bulletin F900EX-414, except for airplanes modified in service with any of the service information specified in paragraphs (c)(2)(i) through (c)(2)(vii) of this AD. (i) Dassault Aviation Service Bulletin F900EX-400, dated July 1, 2011. (ii) Dassault Aviation Service Bulletin F900EX-400, Revision 1, dated July 5, 2012. (iii) Dassault Aviation Service Bulletin F900EX-400, Revision 2, dated November 30, 2012. (iv) Dassault Aviation Service Bulletin F900EX-414, dated July 20, 2011. (v) Dassault Aviation Service Bulletin F900EX-414, Revision 1, dated July 5, 2012. (vi) Dassault Aviation Service Bulletin F900EX-414, Revision 2, dated July 27, 2012. (vii) Dassault Aviation Service Bulletin F900EX-414, Revision 3, dated November 30, 2012. (3) Dassault Aviation Model FALCON 2000EX airplanes, all serial numbers, except airplanes with Dassault Aviation production modification M3254, or modified in service by Dassault Aviation Service Bulletin F2000EX-300 (“EASy II” avionics).

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 normal procedures and limitations sections of the AFM, as applicable, to include new yaw damper procedures, in accordance with using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA.

Unsafe condition

This AD was prompted by a report that during a test flight, it was found that the yaw damper on the takeoff roll can increase the Minimum Control Speed on Ground (Vmcg). We are issuing this AD to ensure that the flightcrew has procedures to set the yaw damper to “off” before takeoff, which, if activated, could result in reduced control of the airplane if one engine were to fail during takeoff.

Affected ADs

None.

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