EasyManua.ls Logo

Gulfstream G200 - System Controls and Indicators

Gulfstream G200
13 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...
SLATS/FLAPS SYSTEM CONTROLS
AND INDICATORS
SLATS/KRUEGER/FLAPS Control Lever - Has five positions as
follows:
UP - Flaps, krueger flaps and slats are up.
DN - Slats and krueger flaps are extended, flaps stay
retracted
12°; 20°; 40°; - Slats and krueger flaps stay extended.
Flaps are extended, as required for the particular
operation (take-off, approach or landing)
SLAT BYPASS ARM Pushbutton - Used to stop and bypass slats
operation if failure occurs to slats extension/retraction
system
FLAP/SLAT TEST Switch (on pedestal side) - This switch is used to
test the slats/flaps controller. The switch is spring loaded to center
(ON) position. Placing the switch in TEST position, tests all of the
system components (SLATS/FLAPS position transmitters, drive
disconnect switches, oleo switch connection, up/down limit switches
and slats/flaps monitor power supply). OFF/RESET position stops the
test and reset the system.
This switch
is intended only for maintenance checks.
Aural Warnings
Overspeed Sound - Aural warning sounds when slats, flaps and
krueger flaps are not fully retracted and airspeed above
250 KIAS/ 0.55M
Gulfstream G200 - Trim System
Page 11

Related product manuals