Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 689

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
NORMAL PROCEDURES
PREFLIGHT INSPECTION

External Inspection (See Preflight Checks in Limitations)
1. Wings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
2. Horizontal Stabilizer . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
3. Vertical Stabilizer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
4. Windshield . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Conduct a visual and tactile inspection of all critical
surfaces in accordance with the Limitations Section
of this supplement, to make sure complete removal
of contamination.
5. TKS Ice Protection System Fluid Tank . . . . CHECK QUANTITY
The airplane must be level to assure accurate TKS Ice
Protection System fluid quantity when using the fluid
tank sight gage on the TKS Ice Protection System tank.
6. Porous Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition, security and even distribution of fluid flow from
all panels)
Look for signs of TKS Ice Protection System fluid
leakage through bonded area of the porous panels. If
TKS Ice Protection System fluid is leaking through the
bonded seam do not operate the TKS Ice Protection
System.
7. Propeller . . . . . . . . . . . . . . . . . . . . . CHECK FOR FLUID FLOW
8. Windshield Spray Bar . . . . . . . . . . . . . . . . CHECK CONDITION
9. Stall Warning Vane . . . . . . . . . . . . . . . . PERCEPTIBLY WARM
10. PITOT/STATIC Tubes . . . . . . . . . . . CLEAR AND VERY WARM
11. Static Wicks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
FAA APPROVED
208BPHCUS-S1-00
SECTION 9 - SUPPLEMENTS
(Continued)
(Continued)
WARNING
CAUTION
CAUTION
(verify condition and security)
SUPPLEMENT 1
and CAP SECURED
(Min. 11.7 U.S. gallons)
U.S.
S1-37