CESSNA
MODEL 208B G1000
GARMIN G1000
NORMAL PROCEDURES
BEFORE LANDING
1. AIR CONDITIONING Switch. . . . . . . . . . . . OFF or VENTILATE
(if takeoff torque under landing conditions would be set below
2397 FT-LBS)
AFTER LANDING
1. AIR CONDITIONING Switch. . . . . . . . . . . . . . . . . AS DESIRED
PERFORMANCE
There is a 25 FPM reduction in climb performance, 1 to 2 KTAS
decrease in cruise performance, and approximately 1% increase in fuel
required for a given trip as a result of the air conditioner installation.
This reduction in climb and cruise performance may be eliminated by
installation of the condenser duct inlet and exit cover plates during
flights when the air conditioner will not be used.
When the air conditioner is operating (compressor engaged), the
following additional performance changes are also applicable:
TAKEOFF
The air conditioner installation has no appreciable effect on takeoff
distances.
FAA APPROVED
208BPHCUS-S7-00
SECTION 9 - SUPPLEMENTS
(Continued)
U.S.
SUPPLEMENT 7
S7-11