67-27-01 AVIONS MARCEL DASSAULT: Amdt. 39-474, Part 39, Federal Register September 9, 1967. Applies to Fan Jet Falcon Airplanes, Serial Numbers 1 thru 94.
Compliance required within the next 200 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent jamming of the engine power lever, modify the type MF 2006 pressurization control microswitch installation by the addition of a support, P/N MY.20.240.3801, and a leaf spring, P/N MY.20.240.3802, in accordance with Avions Marcel Dassault Service Bulletin No. 211, (76-4), revision 1, dated April 4, 1967, or later SGAC-approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region.
This amendment effective October 9, 1967.