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SECTION 4
NORMAL PROCEDURES
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
4. Touchdown . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST
5. POWER Lever. . . . . . . . BETA RANGE AFTER TOUCHDOWN
6. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAXIMUM
7. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
BALKED LANDING
1. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE
2. WING FLAPS Handle . . . . . . . . . . . . . . RETRACT to TO/APR
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS MINIMUM
4. ELEVATOR TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRIM
5. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . RETRACT
6. ELEVATOR TRIM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRIM
4-40
(while holding elevator control full aft)
(for maximum brake effectiveness)
(after reaching safe altitude and airspeed)
U.S.
MODEL 208B 867 SHP
GARMIN G1000
(after clearing obstacles)
(for takeoff power)
(until obstacles are cleared)
FAA APPROVED
208BPHCUS-00
CESSNA
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