CESSNA SECTION 3
MODEL 208B 867 SHP ABNORMAL PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
ENGINE
AMBER CHIP DETECT ANNUNCIATOR COMES ON
1. Engine Indicating System . . . . . . . . . . CHECK PARAMETERS
(verify within normal operating range)
IF ENGINE INDICATIONS ARE OUTSIDE NORMAL OPERATING
RANGE
2. Reduce power and monitor engine parameters.
3. Land as soon as possible. (refer to ENGINE FAILURE DURING
FLIGHT and EMERGENCY LANDING WITHOUT ENGINE
POWER)
IF ENGINE INDICATIONS ARE WITHIN NORMAL OPERATING
RANGE
2. Continue flight as planned while monitoring engine parameters.
3. Have system inspected by qualified personnel before next flight.
WHITE IGNITION ON ANNUNCIATOR COMES ON
1. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
IF CONDITIONS DO NOT WARRANT ITS USE
2. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
AMBER EMERG PWR LVR ANNUNCIATOR COMES ON
DURING FLIGHT
1. EMERGENCY POWER Lever . . . . . . . . . . . . . . . . . . . CHECK
(verify lever in NORMAL position)
208BPHCUS-00 3-89