Kodiak 100 Series Information Manual page 384

Uncontrolled if printed
S e c t i o n 7
AIRPLANE & SYSTEMS DESCRIPTIONS
Warning Annunciations
Warning annunciations are displayed in
aural alert which chimes intermittently until the pilot acknowledges it by
pressing the ADVISORY softkey. A warning annunciation requires immediate
corrective action and threatens the continued flight of the aircraft.
Annunciation
Window Text
OIL PRESS LOW
FUEL OFF L-R
OVERSPD WARN
CARGO DOOR
RESERVOIR FUEL
CHIP DETECTOR
FLAP OVERSPEED
ITT
NG OVERSPEED
NP OVERSPEED
TORQUE
INLET NOT BP
7-14 0
D O N OT U S E FO R FL I G H T O PE R AT I O N S
Annunciation Description
Activation warns that the low oil pressure threshold has been
crossed. The threshold for activation is 43 PSI with decreasing
pressure. The annunciation will continue to be shown until the
pressure increases to above 75 PSI.
Warns the pilot that both fuel selector valves are in the OFF
position. A red LED light located above the pilot's PFD will also
illuminate and remain illuminated until one or both fuel selector
valves are returned to the ON position.
Warns the pilot that Vmo has been exceeded. The overspeed
warning limits are 182 KIAS with an increasing airspeed and 181
KIAS with decreasing airspeed.
Warns the pilot that the cargo door is not fully closed while the
aircraft is in the air with a groundspeed of at least 30 knots (GPS)
or airspeed of at least 50 knots (TAS).
Warns that the fuel level in the fuel reservoir is low and fuel
starvation is imminent.
Warns the pilot that a metallic chip has been detected in the
reduction gearbox. Pilot action is to continue flight with reduced
power to the nearest available airport.
Warns the pilot that the maximum flap speed for the current flap
position is being exceeded. Pilot action is to reduce airspeed below
the current flap position.
Warns the pilot that the ITT limit is being exceeded. 790°C during
flight or 1090°C during start. Pilot action is to reduce power or bring
the fuel condition lever to CUTOFF (during start).
Warns the pilot that the n
action is to reduce power.
Warns the pilot that the n
Pilot action is to reduce propeller RPM.
Warns the pilot that the takeoff torque limit is being exceeded. Pilot
action is to reduce torque.
Warns the pilot that the engine inlet has failed to reach the BYPASS
position after 18 seconds or more has passed since the Inertial
Particle Separator was switched to BYPASS, indicating either that
the actuating system failed, or that both bypass position indicating
sensors have failed.
RED and are accompanied by an
limit of 101.6 % is being exceeded. Pilot
g
limit of 2200 RPM is being exceeded.
p
P i l o t 's O p e r a t i n g H a n d b o o k
1 0 0 S E R I E S