Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 776

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 7
EMERGENCY PROCEDURES
There is no change to the airplane emergency procedures when the Air
Conditioning System is installed.
NORMAL PROCEDURES
PREFLIGHT INSPECTION
During the preflight (walk around) inspection, open cabin doors to aid in
cool-down of the cabin before flight. Air conditioning system
components should be inspected as follows:
1. Compressor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
2. Drive Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
3. Hoses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
Check hoses for evidence of damage or leaks from compressor
to the condenser and evaporators.
4. Condenser Inlet/Outlet . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
U.S.
S7-8
(on lower left side of cowling)
Check for installation, condition, and blockage.
MODEL 208B 867 SHP
GARMIN G1000
(verify condition)
(verify condition and tension)
FAA APPROVED
208BPHCUS-S7-00
CESSNA