Saab 340B, Operation Manual, Page: 543 / 670

ICE AND RAIN PROTECTION
Description
Aircraft Operations Manual
11.1
PAGE 17
Jun 01/17
A9669
A B
L BETA R BETA
L PROP
DE − ICE
R PROP
DE − ICE
L ENG
ANTI − ICE
R ENG
ANTI − ICE
L/R ENGINE anti − ice switch.
Controls both electrical and bleed air sections of
the engine anti − ice system and illuminates the
ENG ANTI − ICE light in the Flight Status Panel.
L/R AC GEN light (amber).
Will come on if the generator fails.
L/R AC GEN switch.
Controls AC generator power supply.
ON: − AC generator on line.
− Automatic power transfer from
other side in case of generator fail-
ure (except for intake heating).
− No power transfer in case of gener-
ator control failure.
− No power transfer in case of failure
in power feeder line to 115 VAC
GEN BUS.
LOAD XFR − Power transfer from other side.
− Intake heat supplied by own gener-
ator
OFF/R − Off reset position.
− Power transfer from other side.
− No intake heat.
L/R PROP DE − ICE light (blue).
Will come on when the system is working and will
go out in case of system failure.
L/R ENG ANTI − ICE light (blue).
Will come on whenever the engine anti − ice switch
is turned on. With the optional ice detector system
(Mod No 1933) installed the lights come on flash-
ing when ice is detected. With the Eng anti − ice
switched on the lights change to steady indica-
tion.
L/R INTAKE light (amber).
Will come on for a failure in the engine duct electrical
anti − icing systems.
L/R AIR light (amber).
Will come on under the following conditions:
− If the Electronic Solenoid Valve does not open when
respective ENGINE anti − ice switch is turned ON.
− If the Electronic Solenoid Valve does not close when
respective ENGINE anti − ice switch is turned OFF.
A ENGINE ANTI − ICE PANEL
B FLIGHT STATUS PANEL
Fig. 7 Engine anti − ice system − controls and indicators