EasyManua.ls Logo

sonaca aircraft S201 - Instrument Panel

Default Icon
283 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
S201 AFM
7 - AIRPLANE AND SYSTEMS
DESCRIPTION
7.4 - FLIGHT CONTROLS
27/06/2019
SONAIR-S2-D-MAN-006
Rev. : A
7.4.6 FLAP CONTROL
Wing flaps are electrically controlled by a four-position lever located on the
instrument panel (refer to paragraph 7.5). A mechanical flap indicator located
next to the lever shows the current flap position.
The flap motor is located in the cabin centre console. The two wing flaps are
interconnected via a torque tube, which is driven at a single point by the flap
motor. In case of a failure in the linkage system, this prevents the flaps from
being deployed to asymmetrical positions.
See section 7.5 for the location of the flap lever and indicator location on the
instrument panel.

Table of Contents

Other manuals for sonaca aircraft S201