Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 677

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
EMERGENCY PROCEDURES
INERTIAL SEPARATOR MALFUNCTION
1. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . . . . BYPASS
If the INERTIAL SEPARATOR is set to BYPASS at any
point due to suspected or actual icing conditions, do not
return it to NORMAL until the inertial separator door has
been visually inspected and verified free of ice and ice
protection fluid.
2. Engine TRQ Indicator . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
(torque redline and torque bug should drop approximately 100 to
200 foot-pounds)
IF INERTIAL SEPARATOR FAILS TO MOVE TO BYPASS
3. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
4. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
PROPELLER ANTI-ICE SYSTEM MALFUNCTION
IF UNEVEN OR INADEQUATE ANTI-ICING OF THE PROPELLER
BLADES IS INDICATED BY EXCESSIVE VIBRATION
1. A-ICE Annunciator . . . . . . . . . . . . . . VERIFY NORM OR HIGH
2. PROP RPM Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE
IF EXCESSIVE PROPELLER VIBRATION CONTINUES
3. MAX FLOW Switch . . . . . . . . . . . . . . . . . . . . . . . . . AIRFRAME
4. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
FAA APPROVED
208BPHCUS-S1-00
SECTION 9 - SUPPLEMENTS
(Continued)
(rotate counterclockwise and PULL out)
CAUTION
(PRIMARY Switch in NORM or HIGH)
(MAX to MIN and return to MAX)
SUPPLEMENT 1
S1-25
U.S.