Textron Cessna Grand Caravan Ex 208B - Page 211

CESSNA SECTION 3
MODEL 208B 867 SHP ABNORMAL PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
ICE AND RAIN PROTECTION (Continued)
AMBER L, R OR L-R P/S HEAT ANNUNCIATOR COMES
ON
(Continued)
IF COPILOT PFD AND STANDBY ALTIMETER AGREE (PILOT
PFD DIFFERS)
c. SENSOR Softkey (Pilot PFD). . . . . . . . . . . . . . . . . . PRESS
d. ADC2 Softkey. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
e. PFD ADI Displays . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
(amber BOTH ON ADC2 is displayed on both PFDs)
IF PILOT PFD AND STANDBY ALTIMETER AGREE (COPILOT
PFD DIFFERS)
c. Autopilot ALT Mode . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
(disengage altitude hold mode)
d. ALT STATIC AIR Control Knob. . . . . . . . . . . . . . . PULL ON
NOTE
The alternate static source is connected to the pilot’s PFD
and standby instruments only. Refer to Section 5,
Performance, Figure 5-1 (Sheet 2), Airspeed Calibration,
Alternate Static Source correction chart and Figure 5-2,
Altimeter Correction, Alternate Static Source correction
chart for airspeed and altimeter corrections.
(Continued Next Page)
208BPHCUS-00 3-95