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SECTION 3 CESSNA ABNORMAL PROCEDURES MODEL 208B G1000 LOWER HALF OF PASSENGER AIRSTAIR DOOR OPEN 1. Airspeed . . . . . . . . . . . . . . . MAINTAIN LESS THAN 100 KIAS 2. Flight Controls . . . . . . . . . . MANEUVER (for return for landing) 3. WING FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL 4. Approach. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL 5. Landing . . . . . . . SLIGHTLY TAIL LOW (avoid nose high flare) RIGHT OR LEFT CREW DOORS OPEN 1. Airspeed . . . . . . . . . . . . . . . MAINTAIN LESS THAN 125 KIAS 2. Door . . . . . . . . . . . . . . . . . . . . . . . PULL CLOSED and LATCH CARGO POD DOOR(S) OPEN 1. Airspeed . . . . . . . . . . . . . . . MAINTAIN LESS THAN 125 KIAS 2. Land . . . . . . . . . . . . . . . . . . . . . . . AS SOON AS PRACTICAL a. Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL b. Landing . . . . . . . . . . . . . . . . AVOID A NOSE HIGH FLARE ELECTRICAL STARTER CONTACTOR DOES NOT DISENGAGE AFTER START (Amber STARTER ON CAS MSG) 1. Battery Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF 2. External Power Unit . . . . . . . . . . . . . . OFF, then DISENGAGE 3. Fuel Condition Lever. . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF 4. Engine Shutdown . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE GENERATOR LOAD ABOVE LIMIT (Amber GENERATOR AMPS CAS MSG) 1. GEN AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK If amperes are above limit: 2. Electrical Load. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE ALTERNATOR LOAD ABOVE LIMIT (Amber ALTNR AMPS CAS MSG) 1. ALT AMPS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK If amperes are above limit: 2. Electrical Load. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE 3-68 U.S. FAA APPROVED 208BPHBUS-01
CESSNA SECTION 3 MODEL 208B G1000 ABNORMAL PROCEDURES STANDBY POWER INOPERATIVE (Amber STBY PWR INOP CAS MSG) 1. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . CHECK ON IF CAS MESSAGE REMAINS: 2. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . OFF, THEN ON NOTE If the STBY ALT PWR CAS MSG remains, the alternator system may still be operational. A bus voltage surge may have temporarily tripped the ACU (alternator control unit). The ACU can be restored by cycling the STBY ALT PWR Switch. IF CAS MESSAGE STILL REMAINS: 3. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Complete flight using generator power only. Avoid icing conditions. STANDBY POWER ON (White STBY PWR ON CAS MSG) NOTE • During ground operations with CONDITION Lever at LOW IDLE, it is possible that a generator underspeed condition may occur allowing the standby alternator to automatically assist with the electrical load. In this case advance the CONDITION Lever to HIGH IDLE to increase engine speed and bring the generator online. • The Standby Alternator Power may have automaticaly turned on due to a failure of antoher system. Address any Red or Amber CAS MSGs that are present. FAA APPROVED 208BPHBUS-01 U.S. 3-69
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CESSNA INTRODUCTION MODEL 208B G100
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CESSNA SECTION 1 MODEL 208B G1000 G
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CESSNA SECTION 2 MODEL 208B G1000 L
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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CESSNA SECTION 4 MODEL 208B G1000 N
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CESSNA SECTION 5 MODEL 208B G1000 P
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CESSNA SECTION 6 MODEL 208B G1000 W
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CESSNA SECTION 7 MODEL 208B G1000 A
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SECTION 7 CESSNA AIRPLANE AND SYSTE
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CESSNA SECTION 8 MODEL 208B G1000 H
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