EasyManua.ls Logo

Cessna 208B - Center of Gravity Limits; Maneuverlimits; Weight Limits

Cessna 208B
488 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
CESSNA
MODEL
2088 (675 SHP)
SECTION 2
LIMITATIONS
WEIGHT LIMITS
Maximum Ramp Weight: 8785 lbs.
Maximum Takeoff Weight: 8750 lbs.
Maximum Landing Weight: 8500 lbs
Maximum Weight for Flight into Known Icing Conditions:
Cargo Pod Installed: 8550
lbs.
Cargo Pod Removed: 8750 lbs.
NOTE
Refer to Section 6 of this handbook for recommended
loading arrangements in the Standard 208 and
Cargomaster.
CENTER
OF
GRAVITY
LIMITS
Center of Gravity Range:
Forward:
179.60 inches (3.06% MAC) aft of datum at 5500
lbs
or less, with straight line variation to 193.37 inches
(23.80% MAC) aft of datum at 8000 lbs, and straight
line variation to 199.15 inches (32.50% MAC) aft of
datum at 8750 lbs.
AR:
204.35 inches (40.33% MAC) aft of datum at all
weights up to 8750 lbs.
-,
Reference Datum: 100 inches fornard of front face of firewall
Mean Aerodynamic Chord (MAC):
The leading edge of the MAC is 177.57 inches afl of the datum. The
MAC length is 66.40 inches.
MANEUVER LIMITS
Th s airplane
s
cert ficated in tne normal category. The normal category
is
aDDllcable to a rcrafl intended for non-aerobatc operations. Tnese
include any maneuvers incidental to normal flying,
st'alls (except whip
stalls), lazy eights, chandelles, and turns in which the angle of bank is
-)
not more than 60".
Aerobatic maneuvers, including spins, are not approved.
-,
FAA
APPROVED
1
Revision 23

Table of Contents

Related product manuals