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Section11
BEECHCRAFTSundowner180
Limitations
C23
(M-1285
and After)
UTILITY/ACROBATIC CATEGORY
Forward:
107.8
inches
aft of datum
to 1800
lbs with
straight
line variation
to 110.2
inches
aft of
datum
at 2030
lbs.
Aft:
114.0
inches
aft
of
datum
at all weights.
REFERENCE
DATUM
Datum
is 103 inches
forward of
wing leading
edge.
MAC length
is
52.7
inches.
MANEUVER LIMITS
This
airplane
is
approved
for
4 place
in the
Normal
Category
and for
2 place
in the
Utility and Acrobatic
Category.
Maximum
slip duration
is
30
seconds.
NORMAL CATEGÓRY (2450
POUNDS)
No acrobatic
maneuvers
approved.
UTILITY CATEGORY (2030
POUNDS)
No acrobatic
maneuvers
are approved
except those
listed
below.
MANEUVER
ENTRY SPEED
(CAS)
Chandelle
......................
116
kts/133
mph
Steep
Turn
.....................
116 kts/133
mph
Lazy Eight
......................
116 kts/133
mph
Stall (Except Whip)
.........
Use
slow
deceleration
Intentional
Spins
M-1494 and
after (only if certificated
as
Acrobatic}
or
prior
airplanes
modified
by
Kit No. 23-4007-15
per
S.I. No.
0619-090
.
.
.
.
.
.
.
.
.
.
.
.
Use
slow
deceleration
IACROBATIC CATEGORY
(2030
POUNDS)
For additional
approved
acrobatic
maneuvers, see
FAA
Approved
Airplane
Flight Manual Supplement.
2-8
Revised:
October
1979
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