67-27-01: Engine Power Lever

FAA order 67-27-01 is an airworthiness directive in force since October 9, 1967. The FAA's subject line: Engine Power Lever. It names Dassault/Sud FAN JET FALCON: about 24 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product: Aircraft
Makes: Dassault Aviation
Models: Fan Jet Falcon
On this site: Dassault/Sud FAN JET FALCON 24 registered

Dates and paperwork

In force since: October 9, 1967
Docket: Unknown
Status: Current
The FAA's document: Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (803 characters)

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.

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 2, 2026. Connections as data: /graph/directive/67-27-01.json · aircraft systems.