Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 679

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
EMERGENCY PROCEDURES
AMBER L P/S HEAT, R P/S HEAT OR L-R P/S HEAT
ANNUNCIATOR COMES ON
1. PITOT HEAT Circuit Breakers (L and R) . . . . . . . . . . . CHECK
2. Icing Conditions . . . . . . . . . . . . . . . . . . . . EXIT IMMEDIATELY
Do not rely on the Low Airspeed Awareness
System if L P/S HEAT or L-R P/S HEAT annunciator
comes on.
IF AMBER L P/S HEAT OR R P/S HEAT ANNUNCIATOR SHOWN ON
PFD
3. SENSOR Softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
4. ADC 1/2 Softkey . . . . . . . . . . . . SELECT OPPOSITE SYSTEM
5. PFD ADI Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
IF AMBER L-R P/S HEAT ANNUNCIATOR SHOWN ON PFD
3. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISENGAGE
4. ALT STATIC AIR Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
The alternate static source is connected to the pilot side Air
Data Computer (ADC1) and standby instruments only.
Refer to POH/AFM, Section 5, Performance, Figure 5-1
(Sheet 2), Airspeed Calibration, and Figure 5-2, Altimeter
Correction, for Alternate Static Source airspeed and
altimeter corrections.
5. Airspeed . . . . . . . . . . . . EXPECT UNRELIABLE INDICATIONS
6. Fly the airplane using attitude, altitude, and power instruments.
FAA APPROVED
208BPHCUS-S1-00
(first and second row, third breaker from aft end)
WARNING
(amber BOTH ON ADC 1 or 2 shown on both PFDs)
NOTE
SECTION 9 - SUPPLEMENTS
SUPPLEMENT 1
(Continued)
(verify both circuit breakers are IN)
U.S.
(pull full out)
S1-27