Weight Limits; Center Of Gravity Limits - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

CESSNA
MODEL 208B (867 SHP)
GARMIN G1000

WEIGHT LIMITS

Maximum Ramp Weight . . . . . . . . . . . . . . . .8842 Pounds (4010 kg)
Maximum Takeoff Weight . . . . . . . . . . . . . . .8807 Pounds (3994 kg)
Maximum Landing Weight. . . . . . . . . . . . . . .8500 Pounds (3855 kg)
Refer to Section 6, Weight and Balance, Figure 6-11, Cabin
Internal Loading Arrangements, for recommended loading
arrangements.

CENTER OF GRAVITY LIMITS

CENTER OF GRAVITY RANGE
FORWARD WITH OR WITHOUT CARGO POD
185.00 inches (4699 mm) (11.19% MAC) aft of datum at 6500
pounds (2948 kg) or less, with straight line variation to 193.37 inches
(4912 mm) (23.80% MAC) aft of datum at 8000 pounds (3628 kg)
and straight line variation to 199.15 inches (5059 mm) (32.50%
MAC) aft of datum at 8807 pounds (3994 kg).
AFT WITH OR WITHOUT CARGO POD
204.35 inches (5190 mm) (40.33% MAC) aft of datum at all weights
up to 8807 pounds (3994 kg).
REFERENCE DATUM
100 inches (2540 mm) forward of front face of firewall.
MEAN AERODYNAMIC CHORD (MAC)
The leading edge of the MAC is 177.57 inches (4510 mm) aft of the
datum. The MAC length is 66.40 inches (1686 mm).
FAA APPROVED
208BPHCUS-00
OPERATING LIMITATIONS
NOTE
SECTION 2
2-13
U.S.