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BEECHCRAFTSundowner180
Section11
C23 (M-1285 and After)
Limitations
On
Left Door
or
Left
Side
Panel (Acrobatic): (M-1971, M-
1980
and after) (CAS)
THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE
WITH THE
OPERATING LIMITATIONS
STATED IN THE
FORM OF
PLACARDS, MARKINGS
AND
MANUALS.
NORMAL CATEGORY
MAX1MUM
DESIGN
WEIGHT
2450
LBS
REFER
TO
WEiGHT
AND
BALANCE
DATA
FOR LOADING
INSTRUCTIONS
FLIGHT
MANEUVERING
LOAD FACTOR
FLAPS UP
+3.8
-1.9
DOWN
+1.9
MAXIMUM MANEUVERING
SPEED
118 KTS/136
MPH
NO
ACROBATIC
MANEUVERS
INCLUDING
SPINS
APPROVED
UTILITY&
ACROBATIC
CATEGORY
MAXIMUM
DESIGN
WEIGHT
2030
LBS
REFER TO WEIGHT
AND BALANCE
DATA
FOR LOADING
INSTRUCTIONS
FLIGHTMANEUVERING
LOAD FACTOR
FLAPS UP
+6.0
--30
DOWN
+2.0
NO
ACROBATIC
MANEUVERS
APPROVED
EXCEPT THOSE LISTED BELOW:
MANEUVER
MAXIMUM
ENTRY SPEED
CHANDELLES
116 KTS/133
MPH
LAZY EIGHTS
116 KTS/133
MPH
STEEP
TURNS
116 KTS/133
MPH
STALLS lEXCEPT
WHIP
STALLS)
SLOW
DECELERATION
NOTE: MAXIMUM
ALTiTUDE LOSS
DURING
STALL
300
FT
SPINS IFOR OPERATIONAL
LIMITATIONS
SEE PLACARD ON
$UN VISOR)
RECOMMENDED
ENTRY SPEED
BARREL ROLL
113 KTS/130
MPH
AILERON
ROLL
113 KTS/130
MPH
SNAP
ROLL
87
KTS/100
MPH
SPLIT 5
79
KTS/90
MPH
IMMELMANN
130
KTS/150
MPH
LOOP
122
KTS/140
MPH
On
Right Side
of
Instrument
Panel (Acrobatic)
CAUTION
CONTINUOUS
INVERTED
FLIGHT WILL CAU5E
LOSS OF OIL AND OIL PRESSURE.
REAR CG
LIMITED AND
CARRYING
OF BAGGAGE
OR
REAR SEAT PASSENGERS
AND USE OF
FLAPS PROHIBITED
DURING
ACROBATIC
MANEUVERS.
February
1979
2-23
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