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SECTION 3 CESSNA ABNORMAL PROCEDURES MODEL 208B G1000 PITOT STATIC HEATER FAILURE (Amber L, R OR L-R P/S HEATER CAS MSG) (Continued) IF UNABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE 1. Land as soon as practical. Consider diversion to visual conditions. 2. Maintain altitudes based on LOWEST indicated altitude. 3. ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVISE (of inability to verify correct altitude) 4. If unable to descend into visual conditions, plan ILS approach with course intercept well outside the Final Approach Fix (FAF). 5. Once glideslope is captured, determine most accurate altitude source when crossing FAF. 6. Reference ILS Decision Height to most accurate altimeter based on FAF crossing. 3-76 U.S. WARNING TAWS alerts are based on GPS altitude and position information and are independent of ADC data. If a TAWS alert is received, it should be considered valid and appropriate terrain avoidance action should be taken. FAA APPROVED 208BPHBUS-01
CESSNA SECTION 3 MODEL 208B G1000 ABNORMAL PROCEDURES STALL HEAT FAILURE (Amber STALL HEAT CAS MSG) If ice is observed forming on the stall warning vane or its mounting plate: 1. STALL WARN Circuit Breaker . . . . . . . . . . . . . . . . . . . CHECK (verify circuit breaker is IN) CAUTION With continued ice buildup, expect no stall warning horn during slow speed operation. The autopilot will not automatically disconnect during a stall with out the stall warning vane working properly. 2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR NOTE Do not rely on the stall warning system. Maintain airspeed in accordance with the minimum speed for icing conditions in Section 2, Limitations of this supplement. MISCELLANEOUS EMERGENCY DESCENT PROCEDURES ROUGH AIR 1. Seats, Seat Belts, Shoulder Harnesses . . . . . . . . . . . SECURE 2. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE 3. PROP RPM Lever. . . . . . . . . . . . . . . . . . . . . MAX (full forward) 4. WING FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP 5. Weights and Airspeed: 8750 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . 148 KIAS 7500 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . 137 KIAS 6250 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . 125 KIAS 5000 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . 112 KIAS SMOOTH AIR 1. Seats, Seat Belts, Shoulder Harnesses . . . . . . . . . . . SECURE 2. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE 3. PROP RPM Lever. . . . . . . . . . . . . . . . . . . . . MAX (full forward) 4. WING FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10° 5. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 175 KIAS FAA APPROVED 208BPHBUS-01 U.S. 3-77
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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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