BEECHCRAFT
Debonair
C33
Bonanza
E33
and
F33
Section
II
Limitation&
1,
CENTER OF
GRAVITV
LIMITS
(Gear
Down)
'·-·
Forward:
77.0
inches
aft
of
datum to
2700
lbs
with
straight line variation to 81.5 inches at
3050
lbs.
Aft: 86. 7 inches aft of
datum
at all weights.
REFERENCE
DATUM
Datum is 83.1 inches forward of center line through
forward jack points.
MAC leading edge is 66. 7 inches
aft
of
datum.
MAC
length
is
65.3 inches.
MANEUVER
LIMITS
This is a utility category airplane. Spins are prohibited. No
acrobatic maneuvers are approved except those
listed
below. Maximum slip duration is
30
seconds for airplanes
with
baffledmain
fuel cells in both
wings
and
20
seconds
for airplanes
with
unbaffled main fuel cells
in
either wing.
APPROVED
MANEUVERS
(3050
POUNDS)
MANEUVER
ENTRY
SPEED
(CAS)
Chandelle . . . . . . . . . . . . . . . . . . . . . .
128
kts{147 mph
Steep Turn
........
„
...........
128
kts{147 mph
Lazy
Eight
.......
„
..
„
.....
„ . .
128
kts{147 mph
Stall (Except Whip) . . . . . . . . . Use slow deceleration
Minimum
tue/ for above maneuvers - 10 gallons each
main tank.
Spins are prohibited.
August
1982
2-9
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