SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
LANDING
NORMAL LANDING
1. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . LAND
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-85 KIAS
3. Touchdown . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST
4. POWER Lever. . . . . . . . BETA RANGE AFTER TOUCHDOWN
5. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY
SHORT FIELD LANDING
1. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . LAND
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78 KIAS
Refer to Section 5, Performance, Figure 5-26 or Figure 5-43,
Short Field Landing Distance for speeds at reduced weights.
3. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . REDUCE to IDLE
(after clearing obstacles)
4. Touchdown . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST
5. POWER Lever. . . . . . . . BETA RANGE AFTER TOUCHDOWN
6. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAXIMUM
(while holding elevator control full aft)
7. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
(for maximum brake effectiveness)
BALKED LANDING
1. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE
(for takeoff power)
2. WING FLAPS Handle . . . . . . . . . . . . . . RETRACT to TO/APR
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS MINIMUM
(until obstacles are cleared)
4. ELEVATOR TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRIM
5. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . RETRACT
(after reaching safe altitude and airspeed)
6. ELEVATOR TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRIM
208BPHCUS-004-40