Textron Cessna Grand Caravan Ex 208B - Page 677

CESSNA SECTION 9 - SUPPLEMENTS
MODEL 208B 867 SHP SUPPLEMENT 1
GARMIN G1000
U.S.
FAA APPROVED
EMERGENCY PROCEDURES (Continued)
INERTIAL SEPARATOR MALFUNCTION
1. INERTIAL SEPARATOR. . . . . . . . . . . . . . . . . . . . . . . . BYPASS
(rotate counterclockwise and PULL out)
CAUTION
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
(PRIMARY Switch in NORM or HIGH)
2. PROP RPM Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE
(MAX to MIN and return to MAX)
IF EXCESSIVE PROPELLER VIBRATION CONTINUES
3. MAX FLOW Switch. . . . . . . . . . . . . . . . . . . . . . . . . AIRFRAME
4. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
S1-25208BPHCUS-S1-00