Airspeeds For Normal Operation - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

SECTION 4
NORMAL PROCEDURES

AIRSPEEDS FOR NORMAL OPERATION

Unless otherwise noted, the following speeds are based on a maximum
takeoff weight of 8807 pounds (3994 kg) and landing weight of 8500
pounds (3855 kg) and may be used for any lesser weight. However, to
achieve the performance specified in Section 5 for takeoff distance,
climb performance, and landing distance, the speed appropriate to the
particular weight must be used.
TAKEOFF
Normal Climb, FLAPS TO/APR . . . . . . . . . . . . . . . . . . 90-100 KIAS
Short Field Takeoff, FLAPS TO/APR, Speed at 50 Feet . . . 86 KIAS
Type II, Type III or Type IV
Anti-ice Fluid Takeoff (FLAPS UP). . . . . . . . . . . . . . . . . . . . 83 KIAS
ENROUTE CLIMB, FLAPS UP
Cruise Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110-120 KIAS
Best Rate of Climb, Sea Level to 3000 Feet . . . . . . . . . . . 108 KIAS
Best Rate of Climb, 20,000 Feet . . . . . . . . . . . . . . . . . . . . . 92 KIAS
Best Angle of Climb, Sea Level to 20,000 Feet . . . . . . . . . . 86 KIAS
LANDING APPROACH
Normal Approach, FLAPS UP . . . . . . . . . . . . . . . . . . 100-115 KIAS
Normal Approach, FLAPS LAND. . . . . . . . . . . . . . . . . . 75-85 KIAS
Short Field Approach, FLAPS LAND . . . . . . . . . . . . . . . . . . 78 KIAS
BALKED LANDING
Takeoff Power, FLAPS TO/APR. . . . . . . . . . . . . . . . . . . . . . 80 KIAS
MAXIMUM
PENETRATION SPEED
8807 POUNDS (3994 kg) . . . . . . . . . . . . . . . . . . . . . . . . . 148 KIAS
7500 POUNDS (3401 kg) . . . . . . . . . . . . . . . . . . . . . . . . . 137 KIAS
6250 POUNDS (2834 kg) . . . . . . . . . . . . . . . . . . . . . . . . . 125 KIAS
5000 POUNDS (2267 kg) . . . . . . . . . . . . . . . . . . . . . . . . . 112 KIAS
MAXIMUM DEMONSTRATED CROSSWIND VELOCITY
Takeoff or Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 KNOTS
4-4
RECOMMENDED
U.S.
CESSNA
MODEL 208B 867 SHP
GARMIN G1000
TURBULENT
FAA APPROVED
208BPHCUS-00
AIR