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SECTION 3 CESSNA ABNORMAL PROCEDURES MODEL 208B G1000 ENGINE GEAR BOX CONTAMINATION (Amber CHIP DETECT CAS MSG) 1. Engine Indications. . . . . . . . . . . . . . . . CAREFULLY MONITOR (for abnormal oil pressure, oil temperature or power indications) CAUTION • If engine indications are normal, proceed to destination and determine cause of Amber CHIP DETECT CAS MSG prior to next flight. • If engine indications confirm Amber CHIP DETECT CAS MSG, proceed in accordance with Engine Failures checklists or at the discretion of the pilot and consistent with safety, continue engine operation in preparation for an emergency landing as soon as possible. IGNITION ON (White IGNITION ON CAS MSG) 1. IGNITION Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IF CONDITIONS WARRANT: 2. IGNITION Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM FLIGHT CONTROLS ASYMMETRIC FLAP EXTENSION OR SUDDEN FLAP RETRACTION ON ONE SIDE 1. 2. Apply aileron and rudder to stop the roll. WING FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP 3. Airspeed . . . . . . . . . . . . . . . . SLOW to 100 KIAS (or less) 4. If both flaps retract to a symmetrical setting: a. Plan a flaps up landing. b. Refer to Section 5 (notes above landing performance tables) for increase in approach speed and landing distance. 5. If both flaps cannot be retracted to a symmetrical setting: a. Land as soon as practical. b. Maintain a minimum airspeed of 90 KIAS on the approach and avoid a nose high flare on landing. 3-70 U.S. FAA APPROVED 208BPHBUS-01
CESSNA SECTION 3 MODEL 208B G1000 ABNORMAL PROCEDURES FLAPS FAIL TO EXTEND OR RETRACT 1. FLAP MOTOR and STBY FLAP MOTOR Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IN 2. If flaps still fail to extend or retract: a. Guarded and Safetied STBY FLAP MOTOR Switch (Overhead) . . . . . . . . . . . . MOVE GUARD, BREAKING SAFETY WIRE, AND POSITION SWITCH TO STBY b. Guarded and Safetied STBY FLAP MOTOR UP/ DOWN Switch (Overhead. . . . . . . . . . . . . . . . . . . . MOVE GUARD, BREAKING SAFETY WIRE, AND POSITION SWITCH UP OR DOWN Hold switch until flaps reach desired position, except release switch before flaps reach full up or full down travel. CAUTION With the standby flap system in use, limit switches which normally shut off the primary flap motor when reaching the flap travel limits are electrically inactivated. Therefore, the pilot must release the standby flap motor up/down switch before the flaps reach their travel limit to prevent overloading and damage to the flap system. 3. Guarded STBY FLAP MOTOR Switch . . . . . . . LEAVE in STBY (until maintenance action can be accomplished) FAA APPROVED 208BPHBUS-01 U.S. 3-71
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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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