Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 663

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
LIMITATIONS
REQUIRED EQUIPMENT
The following equipment must be installed and fully operational for
flight into known or forecast icing conditions:
1. Wing and wing strut leading edge porous panels
2. Horizontal stabilizer leading edge porous panels
3. Vertical stabilizers leading edge porous panels
4. Propeller fluid slinger assembly
5. TKS Ice Protection System equipment pack (tank assembly,
pumps, filters)
6. Windshield spray bar
7. Heated lift detector (stall warning) vane
8. Alternate Static Source
9. Left and Right Pitot/Static Tube Heat System
10. Wing Ice Inspection Light
11. Engine Driven Generator
12. Standby Electrical System
13. Engine Inertial Separator
14. Heater and Defroster
15. Hartzell Propeller: HC-B3TN-3AF/T10890CNB-2
16. Cargo Pod
17. Low Airspeed Awareness System
18. Windshield Ice Detection Light
19. Vortex Generators (10 per wing)
WINDSHIELD PUMP
The windshield pump is rated for intermittent use only. Continuous
operation may damage the pump.
Do not operate the windshield pump continuously
longer than 10 seconds. Allow at least 10 seconds
between operations.
FAA APPROVED
208BPHCUS-S1-00
(Continued)
WARNING
SECTION 9 - SUPPLEMENTS
SUPPLEMENT 1
U.S.
S1-11