Ice And Rain Protection; Amber L, R Or L-R P/S Heat Annunciator Comes On - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

CESSNA
MODEL 208B 867 SHP
GARMIN G1000

ICE AND RAIN PROTECTION

AMBER L, R OR L-R P/S HEAT ANNUNCIATOR COMES
ON
1. LEFT PITOT HEAT and
RIGHT PITOT HEAT Circuit Breakers . . . . . . CLOSE (push in)
2. Icing Conditions . . . . . . . . . . . EXIT AS SOON AS POSSIBLE
IF ICE BEGINS TO FORM NEAR THE STATIC PORT OF THE LEFT
PITOT/STATIC TUBE (FROM COMPENSATION RING TO AFT END
OF TUBE) OR AMBER IAS MISCOMP AND/OR AMBER ALT
MISCOMP MESSAGES COME ON PILOT'S PFDS
3. Pilot and Copilot Airspeed . . . . . . . . . . . . . . . . . . . . COMPARE
The standby airspeed indicator uses the same
pitot-static sources as the pilot's side air data
computer (ADC1). Do not use standby airspeed
indicator as sole source in determining correct
airspeed.
4. Autopilot ALT Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
5. ALT STATIC AIR Control Knob . . . . . . . . . . . . . . . . . . PULL ON
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.
IF STANDBY AIRSPEED AND COPILOT PFD AGREE (PILOT
PFD DIFFERS)
6. SENSOR Softkey (Pilot PFD) . . . . . . . . . . . . . . . . . . . . . PRESS
7. ADC2 Softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
8. PFD ADI Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
FAA APPROVED
208BPHCUS-00
(first and second row, third breaker from forward end)
WARNING
NOTE
(amber BOTH ON ADC2 is displayed on both PFDs)
(Continued Next Page)
ABNORMAL PROCEDURES
(with standby airspeed indicator)
(disengage altitude hold mode)
U.S.
SECTION 3
3-93