Beechcraft C23 SUNDOWNER 180 Pilot Operating Handbook page 41

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BEECHCRAFT
Sundowner
180
Section
II
C23 (M-1285 and After)
Limitations
FUEL QUANTITY
On M-1517
thru
M
1879
except M-1875,
or prior air-
planes
after
compliance
with S.I. No.
0624-281
Yellow Band
........................
E
to
3/8
full
On M-1875, M-1880
and
after
Yellow Band
........................
E
to 1/3 full
WEIGHT
LIMITS
NORMAL CATEGORY
Maximum
Ramp Weight
....................
2455
lbs
Maximum
Take-off
and
Landing
Weight
.......................
2450
lbs
Zero Fuel Weight
.............
No
Structural
Limitation
Maximum
Baggage
Compartment
Load
..........
....
.....................
270
lbs
UTILITY/ACROBATIC
CATEGORY
Maximum Ramp Weight.
.
.
.
.
.
.
.
.
.
.
.
.
.
.
.
.
.2035
lbs
Maximum Take-off
and LandingWeight....................2030Ibs
Zero
Fuel Weight.
.
.
.
.
.
.
.
.
.
.
.
No Structural Limitation
Maximum
Baggage
Compartment
Load
(Utility
Category Only).
.
.
.
.
.
.
.
.
.
.
.
.
.
.270
Ibsi
CENTER
OF GRAVITY
LIMITS
NORMAL CATEGORY
Forward:
107.8
inches
aft of datum
to 1800
lbs with
straight
line variation
to 114.5
inches
at
2450
lbs.
Aft:
118.3
inches
aft of datum
at all weights.
Revised: October 1979
2-7

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