CESSNA
MODEL 208B 867 SHP
GARMIN G1000
AIRPLANE SYSTEMS AND DESCRIPTIONS
TKS
ICE
INDICATION AND MESSAGING
For the four modes of airframe ice protection operation, the resulting
endurance with a full tank of fluid is:
MAXIMUM FLUID ENDURANCE
PRIMARY NORM selected . . . . . . . . . . . . . . . . 3 hours, 25 minutes
PRIMARY HIGH selected . . . . . . . . . . . . . . . . . . 1 hour, 20 minutes
BACKUP selected . . . . . . . . . . . . . . . . . . . . . . . . 1 hour, 20 minutes
MAX FLOW AIRFRAME selected . . . . . . . . . . . . . . . . . . 40 minutes
SYSTEMS ENDURANCE CHARACTERISTICS
FAA APPROVED
208BPHCUS-S1-00
PROTECTION
Figure S1-8
SECTION 9 - SUPPLEMENTS
SUPPLEMENT 1
SYSTEM
OPERATION,
(Continued)
U.S.
(Continued)
S1-67